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�$�$�$��RbLxn5�N�l����n5�$,�$�*�3*"Ln5Z	�u�޵::� �T5Planning Manual for Summer Conferences



Part 1: General Chair
Part 2: Technical Chair


Version 1.0 - August 2000
Part 1

Manual for General Chairs of the Summer Conference






This manual should also work well for planning for Winter Conferences with appropriate changes in dates and schedules.



Manual for General Chairs of the Summer Conference

General Comments

The following manual is written with the summer conference used as an example.  The appendices are also for the summer conference.  However this manual can also be used for the winter conference with obvious changes.  Since there are fewer registrants for the winter conference, this must be taken into account when figuring the budget as in Attachment 2.  The schedule shown in Attachment 3 must also be adjusted for the difference in dates.

Hotel Site

Once the general area for the conference is decided, a letter should be sent to the hotels and other facilities in the area.  A letter should also be sent to the local visitor�s and convention bureau and the chamber of commerce.  This letter should clearly identify the conference along with the number of people expected and what kind of facilities and activities are needed.  A sample letter (used for the Alaska Conference) appears in Attachment 1.

Several proposals from hotels or other facilities at the site should be obtained.  These proposals should include at least the following:

Room rates and number of rooms to be guaranteed/cutoff date of available rooms
Rental for facilities
Rental for a/v equipment
Number and size of room for meetings and number of people that can be held theater style   Setup fees for the rooms
Registration area
Paper sales room
Breakfast setup for speakers� breakfast

If the reception and dinner is to be held at the same site then the following must also be included:

A list of types of food available and the costs
Number of people that the rooms can hold for the type of affair planned and setup fees

Additionally, any activities in the area should also be listed(along with costs(such as:

Hiking trails
Golf
Tours
Etc.

Once a specific proposal is agreed upon, the negotiations with the hotel should include, if possible, a guaranteed price for all rooms and food for the date of the meeting.  Some hotels will do this up to two years in advance and others will simply give the current costs and estimate a percentage increase for the time of the conference.  If the latter is done, then a guarantee of a maximum increase should be obtained.  This makes it easier to do an accurate budget.  If no guarantee is given, another site should be chosen.

As stated above there should be a fixed number of rooms guaranteed.  If possible, it is best to have the date of this commitment on the number of rooms no earlier than several weeks after the Abstract due date.  Allow for the usual one-month abstract date extension. This will allow for a better estimate of the number of attendees as determined by the abstracts submitted and can help in determining overall costs.

If all costs can be defined and guaranteed at the time of signing the contact then this is the best since it allows almost all items to be listed in the preliminary budget and an accurate cost for almost the entire conference can be obtained.

The AAS representative, Carolyn Brown, and not the general chairs should sign the contract.  The contract should also state who is responsible for authorizing additional costs such as additional a/v or room rental, or additional food.  Usually these are the two general chairs.  The contract should also clearly state the number of guaranteed sleeping rooms, the meeting rooms, the food service and all other service provided. Some hotels offer free sleeping rooms for every x number of sleeping rooms filled.  This should be clearly stated in the contract.

Registration and Attendance at Food Affairs

The amount to be charged for registration is the most difficult item to be determined.  The web site offers historical data on attendance by number of members (of AAS or AIAA), nonmembers, and students.  Each are charged a different fee.  Typically 200 registrants (for the summer conference) is a good number to work with but this has varied widely.  The web site should be used to determine this number.  The registration fee can then be determined based on the costs as projected in the budget.

The attendance at the various functions is also difficult to determine.  The early bird reception held on the evening of the first registration will have a lower attendance than the second reception.  There is no historical data for this or for the second reception.  But since the receptions are open to registrants and their families, this additional number must be taken into account.  The chairmen should settle on a number that is guaranteed to the hotel and this is the number that the food is determined from.  This represents the basis for the cost of the reception and is the basis for the cost in the budget.  If the hotel has a good staff for the banquets, they can recommend food that can be increased beyond the guaranteed amount which will not add seriously to the costs.  This means that a contingency may be added to the cost of the reception to allow for growth.

The banquet attendance and cost is determined by the food service and the number of people that can attend.  There is usually a maximum attendance level (due to rooms size, etc.) and since the conference must guarantee a minimum number for which the conference will be charged, this must be done with care or there can be a charge if not enough people attend.  If the cutoff number is set too small, there may be unhappy people.  A cutoff date for the guaranteed attendance near the first or second registration day would be the best for by then, it would be known how many people may attend.  However, this means that there would be no accurate estimate in the budget and this lends some unknown factors in determining the registration fee.  The conference registration fee usually includes a subsidy for the dinner.

Consideration needs to be given to the policy of students, children and other guests (not spouses or significant others) attending the banquet.  Since the banquet is usually subsidized by the registration fee, if there is limited attendance then those conference attendees who cannot go are subsidizing the attendance of outside guests and children. This can be a problem and needs to be addressed with a set policy.

Food and drink is usually the most expensive item on the budget and great care is needed here.  How the chairs handle drinks is also important.  In the past, an open bar was sometimes used but as the costs have increased this has evolved into two free drinks per person.

Budget

A sample budget, used for the Alaska conference is included in Attachment 2.  The budget must include all known costs and a glance at Attachment 2 will show almost all of these.  These include pre-conference costs such as mailings and printings, purchase of supplies, and the cost of advertising the call for papers in the AIAA Journal.  These pre-conference costs are usually paid by the AAS and must be reimbursed.  Some hotels also charge a fee if the food service or drink service is below a certain number and this should be known in advance and included in the budget.  Contingencies for cost growth can be added to the budget in several ways.  Contingencies may be added for each item, such as banquet, reception, A/V equipment, etc.  Or one contingency may be added to the total expected budget.  For Alaska, both were done and it turned out to be too much.  If the hotel guarantees its prices, only a small contingency may be needed.  If the prices are not guaranteed in some areas, a contingency in that area is probably needed.  As seen on the sample budget, the contingency is included in determining the final registration fee.

Schedule of Events

A calendar with a schedule for the completion of various tasks is a very helpful tool to ensure that important items are completed in the proper time frame.  A sample is in Attachment 3.  It is recommended that all chairs, technical and general, have a copy of this schedule and adhere to it as much as possible.

Just Prior to the Conference

A bank account or checking account should be opened with a local bank.  This allows for easy payment of bills, but most importantly for the safe handling of money to be transferred back from the conference.  If this can not be done, then a bank account in the home location of one of the general chairs should be opened.  The checks acquired at the conference can then be mailed back to the account and any cash can either be used to pay bills on site or can be deposited with the hotel for them to write a check that can then be mailed back.

At the Conference

The general chairs should handle the initial registration as problems and questions may arise that have not been previously addressed.  After that, volunteers, or preferably paid helps can handle the registration and paper sales.

As stated, only certain people should be authorized to commit new expenditures with the hotel.

A safe deposit box is a must to store daily receipts prior to deposit in the bank.

All cash should be used to pay hotel bills on site if possible.

Recommendations and Questions to Be Decided.

How many drinks to allow to registrants and how many to accompanying person such as spouses and children?

Do students receive the same benefits (discounts on dinner tickets and drinks) as full paid registrants?

Do accompanying persons receive the same discount on dinner tickets as full paid registrants?
LIST OF ATTACHMENTS


ATTACHMENT 1:		Sample Letter to Hotels 

ATTACHMENT 2:		Sample Budget

ATTACHMENT 3:		Schedule of Events
ATTACHMENT 1- Sample Letter to Hotels

The American Astronautical Society (AAS) would like to hold its annual summer meeting in August of 1999 in Anchorage, Alaska.  I am one of the two General Chairs planning this conference.

The conference typically registers 200+ participants many of whom bring their families since we like to schedule the conference in places that are good for family vacations.  The participants come from government, industry, universities, and from many countries.  Because many of our participants are from government we would like to accommodate them at government rates.

We usually have several receptions at the conference hotel site or nearby.  These receptions consists of finger food and drinks.  We also have a separate evening affair which is usually an informal dinner or cookout.  These events are attended by all registrants and their families.

The conference is run with three parallel sessions, both in the morning and afternoon, with seating in theater style for about 75 to 100 people each.  In addition we need a place to set up the registration desk and a separate room in which we will sell papers that are being presented at the conference.

During the conference days, we have a speakers breakfast each morning for approximately 50 people.  This breakfast usually consists of rolls, muffins, fruit, juice, and coffee.  During the meetings, we have two breaks, one in the morning and one in the afternoon during which coffee and soda is available.

We would normally like to block a number of rooms for our registrants at a guaranteed rate.  If a government rate is available we would like a limited number of rooms at that rate.  If the rooms can be available for 3 days before and after the conference at the conference price, that would also be good since many people like to extend their trip.

If your hotel is interested in being the site for our conference, I would appreciate a proposal from you along with information regarding the hotel.

If there are any questions, I can be reached at my office at the Naval Research Laboratory at:
email:		[email protected]
phone:		202-767-0513
fax:		202-404-7516

home phone:	301-449-7498
home address:	6408 Glen Oak Dr.
		Temple Hills, MD 20748

We will be having our next planning meeting in February 1998 and at that time we will make our final decision on hotels and precise location.  Therefore I would like to have the information well in hand by that time.

Thank you for your prompt reply to this request.
ATTACHMENT 2 - Sample Budget


 EMBED Word.Picture.8  


 EMBED Word.Picture.8  
ATTACHMENT 3 - Schedule of Events

Part 2

Manual for Technical Chairs of the Summer Conference






This manual should also work well for planning for Winter Conferences with appropriate changes in dates and schedules.Manual for Technical Chairs of the Summer Conference


Introduction

The Technical Chairs have overall responsibility for the technical content of the conference.  They determine the scope of the conference and solicit papers through the call for papers.  Based on the submitted abstracts, they assure high technical quality of the conference through their own reviews and subsequent reviews by session chairs.  They are responsible for assembling the conference program complete with all abstracts.  At the conference they ensure that session chairs are present and understand their roles.  They have responsibility for paper sales and collection of papers for the proceedings.

Electronic Processing 

Since the Sun Valley Conference in the summer of 1997, we have made increasing progress toward an all-electronic handling of the technical aspect of the conference.  The process begins with the call for papers.  Authors should be required to supply an email address for all future correspondence.  All subsequent correspondence with authors and session chairs can then occur by email.  Authors should submit both their extended abstract and 100-word abstract electronically.  This facilitates production of the program with abstracts.  

Call for Papers

The first item to be accomplished is the call for papers.  The Technical Chairs should determine the scope of the conference and decide if any special areas will be solicited.  A sample call for papers is included as Attachment 1.  The call for papers should be published in the AIAA Aerospace America magazine as well as the AAS Newsletter in the fall time period.

The number of papers received and accepted will be a major factor in determining the conference schedule.  A large response to the call may allow the conference to be extended to a fourth day.  However, a decision on the length of the conference is subject to dates set by the hotel for changes.  Thus, the deadline for abstract submittal should be early enough to allow ample time to receive all abstracts, review them, and make a final decision on conference length meeting deadlines set by the hotel.  It has been our experience that less than 50% of the abstracts will be received by the announced date.  Typically, we have extended the deadline by 2 to 4 weeks at which point most abstracts will be received.  A timeline of cumulative number of abstracts received for a conference is provided as Attachment 2.

Session Chairs

Session Chairs should be knowledgeable and a recognized contributor in the subject matter of their session.  The primary source of Session Chairs is the membership of the AAS Spaceflight Mechanics and AIAA Astrodynamics Technical Committees.  Volunteers are solicited by passing around a sign-up sheet at the committee meetings.  A sample sign-up sheet is included in Attachment 3.  The sign-up should occur at the committee meetings of the conference prior to the one being worked.

Abstract Review and Selection

Abstracts are sent to the Technical Chairs.  It is recommended that a database be developed as the abstracts are received.  A FilemakerPro progam has been developed for this purpose but a simple spreadsheet also works very nicely.  The data collected should contain:

Author names
Paper title
Corresponding author address including email
Date received

This spreadsheet can be easily manipulated to make session assignments and sequential paper numbering for the program.  An extract from an example spreadsheet is included in Attachment 4.

The Technical Chairs perform an initial review of the papers for technical quality.  Those abstracts that are accepted by the Technical Chairs are assigned to a general topical area, and the number of papers per session is balanced.  It is at this point that the Chairs make an initial assessment of the number of sessions and the length of the conference.  Some flexibility for number of papers presented per day can be gained by the choice of length of paper presentation.  Some conferences have allowed as much as 30 minutes and some have allowed as little as 20 minutes.

After initial review and session assignment, each set of papers is sent to the session chair for a second technical review.  The session chair, being knowledgeable in the subject matter may also recommend that a paper be transferred to another session.  An example letter to session chairs in included in Attachment 5.

After the session chair reviews, the Technical Chair make the final acceptance determination and session assignments.  They then provide to the authors a letter of acceptance or rejection as appropriate.  Acceptance letters also contain explicit instructions on paper preparation and dates for further provision of information to the Chairs.  Sample acceptance and rejection letters are provided in Attachments 6 and 7, respectively.

At this point, a preliminary version of the program, less abstracts, should be posted on the AAS website.

Program

Development and production of the program is also the responsibility of the Technical Chairs.  The most difficult part of this is obtaining 100-word abstracts from every author.  It requires persistence to obtain every last abstract but the satisfaction of a complete program is worth the effort.  Email is invaluable for this task.  After the program is complete, it should be posted on the AAS website in place of the preliminary program posted previously.

Printing of the program is done in various ways.  Some chairs have taken it to a professional printer while others have been able to persuade their parent organization to donate the cost of printing.  Regardless of the source you use, allow ample time so that you can ship the programs to the conference hotel rather than transporting them yourself.

At the Conference

The Technical Chairs have continuing responsibilities at the conference.  These include:

Set up of Technical Paper sales area.  It is recommended that each AAS Paper number be printed in large font on a separate sheet of 8 � X 11 paper.  These should be laid out in order on the paper sales table prior to arrival of the first papers

Receipt of technical papers from authors.  The authors may also provide a camera-ready copy of their paper and possibly a floppy disk.  These should be set aside for later mailing to the proceedings publisher.

Paper Sales.  The Technical Chairs handle the sales of papers.  They provide manning themselves and also recruit others for support.  They should tally sales at the end of each day and secure the funds.  The funds can be turned over to the General Chairs for safekeeping by the hotel.

Speakers� Breakfast.  The Technical Chairs host a speakers� breakfast each morning.  A number of tables should be available corresponding to the number of sessions to be held that day (usually 6).  A sign should be prominently displayed on each table so that speakers can locate their session chair.  Speakers should be reminded of the procedures and time limits for their talks.  This breakfast also affords an opportunity for session chairs to meet authors that they do not know and to obtain bios for authors who have not previously supplied them.

Monitoring Technical Sessions.  Periodically, one of the Technical Chairs should check on the technical sessions to make sure that things are going smoothly.  Problems such as crowded rooms, inadequate heating or cooling, etc. should be quickly and aggressively pursued with the hotel.

Mailing for Proceedings.  At the conclusion of the conference, three copies of each paper should be collected and mailed to the editor of the Proceedings along with the camera-ready copies and disks supplied by the authors. 

Schedule

A typical schedule of actions to be taken is included in Attachment 8.

LIST OF ATTACHMENTS


ATTACHMENT 1:		Conference Call for Papers

ATTACHMENT 2:		Timeline of Cumulative Number of Abstracts Received

ATTACHMENT 3:		Session Chair Volunteer Signup Sheet

ATTACHMENT 4:		Spreadsheet for Technical Program Planning

ATTACHMENT 5:		Initial Instructions to Session Chair

ATTACHMENT 6:		Author Acceptance Letter

ATTACHMENT 7:		Author Rejection Letter

ATTACHMENT 8:		Planning Schedule and Tasks

ATTACHMENT 9:		Foreign Author Letter of Invitation

ATTACHMENT 10:		Technical Paper Cover

ATTACHMENT 11:		Template to use for signs/placards on meeting rooms

ATTACHMENT 12:		Session Chair Reminder Letter

ATTACHMENT 13:		Personal Conference Planner

ATTACHMENT 1

AAS/AIAA Astrodynamics Specialist Conference

August 16-18, 1999

Westin Alyeska Prince Hotel

Girdwood, Alaska (near Anchorage)
 
Abstract Deadline: February 15, 1999

The 1999 Astrodynamics Conference, hosted by the American Astronautical Society (AAS) and cosponsored by the American Institute of Aeronautics and Astronautics (AIAA), will be held August 16-18, 1999 in Girdwood, Alaska, near Anchorage.  The conference is organized by the AAS Space Flight Mechanics Technical Committee and the AIAA Astrodynamics Technical Committee.

	Papers are sought for all areas of astrodynamics.  Topics of interest include, but are not limited to:

Orbital dynamics, perturbations, stability
Trajectory design and optimization
Navigation, guidance and control
Attitude dynamics of rigid and flexible space structures

Papers which contain experimental results or current data are especially encouraged.

	In addition, proposals are solicited for appropriate subjects for special sessions from perspective session organizers.  Areas of interest include, but are not limited to:

Parallel processing applications in astrodynamics
Attitude control and estimation for small satellites
History and future of the US space program
Panel discussions

	Papers will be accepted on the basis of extended abstracts.  The extended abstract must be at least 500-1000 words and should include a description of the problem addressed and the results obtained, as well as a brief summary of the solution procedure and relevance to astrodynamics research.  Abstracts may also contain supporting figures and/or tables.  The abstract must include paper title, names and affiliations of all authors.

	In addition to the extended abstract, you must include the following information to facilitate future correspondence:

Name, affiliation, address, telephone number, fax number and email address for the corresponding author.

	A �no paper-no podium� rule will be in effect for all presentations.  An author will not be permitted to give his or her paper if a written paper has not been prepared and made available at the conference.  AAS will not consider for presentation or publication any paper that has been presented or published elsewhere.  Authors will be required to sign a statement that the paper has not been previously presented or published.

	Special sessions may be as long as four hours on a selected topic.  Their purpose is to invite discussion and the exchange of ideas on �hot topics� in the astrodynamics community and may take a variety of formats, e.g. panel discussions, invited speakers and/or papers, questions and answers, or interactive workshop.  Prospective special session organizers should submit a proposal consisting of a title, a brief description of the session of less than 500 words, and a list of proposed activities and/or invited speakers and titles.

	The American Astronautical Society Space Flight Mechanics Technical Committee also announces the John V. Breakwell Student Travel Award. This award provides a maximum of $1000 to cover travel expenses for U.S. and Canadian students planning to attend the AAS/AIAA Astrodynamics Specialist Conference.  For further details about applications for the award as well as continually updated information concerning the conference, please see the Space Flight Mechanics website at  HYPERLINK http://www.space-flight.org http://www.space-flight.org.

Warning --- Technology Transfer Considerations

	Prospective authors are reminded that technology transfer guidelines have substantially extended the time required for review of abstracts and completed papers by US government agencies.  Internal (company) plus external (government) review can consume 16 weeks or more.  Authors should determine the extent of approval necessary early in the paper preparation process to preclude paper withdrawals and late submissions.

	Two copies of the extended abstract should be submitted to each of the Technical Chairs listed below.  The deadline for submission of the abstract is February 15, 1999.  Formal letters of acceptance with complete instructions will be sent to authors approximately April 10, 1999.
	
AAS Technical Chair
Kathleen Howell
School of Aeronautics and Astronautics
GRIS 1282
Purdue University
West Lafayette, IN 47907-1282
765/494-5786   765/494-0307 FAX
email:  HYPERLINK mailto:[email protected] [email protected]

	AIAA Technical Chair
	Felix Hoots
	GRC International
	Suite 310
	985 Space Center Drive
	Colorado Springs, CO 80915
719/596-5395    719/596-6139 FAX
email:  HYPERLINK mailto:[email protected] [email protected]

AAS General Chair
Bernard Kaufman
Astro Dyn
6408 Glen Oak Dr.
Temple Hills, MD 20748
301/449-7498    301/449-2986 FAX
email:  HYPERLINK mailto:[email protected] [email protected]

AIAA General Chair
Terry Alfriend
Aerospace Engineering Dept.
H.R. Bright Bldg., Room 701
Texas A&M University
College Station, TX 77843-3141
409/845-5920    409/845-6015 FAX
email:  HYPERLINK mailto:[email protected] [email protected]

ATTACHMENT 2
ATTACHMENT 3

Session Chairs

Name				Area of Interest		Address				Phone		E-mail

__________________	__________________	__________________________	__________	__________	

__________________	__________________	__________________________	__________	__________	

__________________	__________________	__________________________	__________	__________	

__________________	__________________	__________________________	__________	__________	

__________________	__________________	__________________________	__________	__________	

__________________	__________________	__________________________	__________	__________	

__________________	__________________	__________________________	__________	__________	

__________________	__________________	__________________________	__________	__________	

__________________	__________________	__________________________	__________	__________	

__________________	__________________	__________________________	__________	__________	

__________________	__________________	__________________________	__________	__________	
ATTACHMENT 4

AUGUST 1999 - AAS/AIAA ASTRODYNAMICS CONFERENCE - ALASKAAAS #No.Rec'dReceipt          E-mailedAuthorTitleAddressesSession #Sess 1Mission Design: Mars - Bob Melton30014403/02/9903/03/99Cesarone, R.J.                                 Hastrup, R.C.                                    Bell, D.J.                                             Roncoli, R.G.Architectural Design for a Mars Communications & Navigation Orbital InfrastructureJet Propulsion Lab, California Institute of Technology, 4800 Oak Grove Dr, Pasadena, CA 91109, [email protected]130110902/26/9903/02/99Kallemeyn, Pieter                            Cangahuala, Alberto                      Ely, Todd; Bell, David                                            Guinn, Joseph                                   Bar-Sever, Yoaz E.                         Lichten, Stephen                             Wu, Sien-Chong                                          Levene, Erik; Vyas, HemaliConstellation Design for a Mars-Orbiting Satellite Communication and Navigation NetworkJet Propulsion Lab, Voice: 818-354-9166, Fax: 818-393-6388, [email protected]13024902/15/99 Willcockson, William H.Mars Polar Lander Entry Descent & Landing DesignLockheed Martin Astronautics, S8800, POB 179, Denver, CO 80201, Voice: 303-977-5094, Fax: 303-977-9345, [email protected]130311102/26/9903/02/99Johnston, M.D.                               Esposito, P.B.                                  Alwar, V.; Demcak, S.W.                                   Graat, E.J.; Burkhart, P.D.                                   Portock, B.M. The Strategy for the Second Phase of Aerobraking Mars Global SurveyorJet Propulsion Lab, California Institute of Technology, 4800 Oak Grove Dr, M/S 264-235, Pasadena, CA 91109, Voice: 818-393-1290, Fax: 818-393-3147, [email protected]130411803/01/9903/02/99Guo, YanpingAladdin's Phasing and Mission Orbit DesignThe Johns Hopkins Univ, APL, Rm 4-141, 11100 Johns Hopkins Rd, Laurel, MD 20723-6099, Voice: 240-228-7541/443-778-7541, Fax: 240-228-1093/443-778-1093, [email protected]130511202/26/9903/02/99Lee, Wayne J.                                    D'Amario, Louis A.                        Roncoli, Ralph B.                            Smith, John C.Mission Design Overview for Mars 2003/2005 Sample Return MissionJet Propulsion Lab, California Institute of Technology, MS 264-380, 4800 Oak Grove Dr, Pasadena, CA 91109, Voice: 818-354-8784, Fax: 818-393-2902, [email protected]130612903/01/9903/03/99D'Amario, Louis A.                     Bollman, Willard E.                          Lee, Wayne J.                                    Roncoli, Ralph B.                             Smith, John C. Mars Orbit Rendevous Strategy for the Mars 2003/2005 Sample Return MissionJet Propulsion Lab, California Institute of Technology, 4800 Oak Grove Dr, MS 301-276, Pasadena, CA 91109, Voice: 818-354-3209, Fax: 818-393-5214, [email protected], [email protected], [email protected], [email protected], [email protected]                               1ATTACHMENT 5

20 March 1997
To:  	Session Chairs for the AAS/AIAA Astrodynamics Conference
	Sun Valley, Idaho

From:  Technical Chairs,
Felix Hoots, AAS
Bernard Kaufman, AIAA

We want to thank you for volunteering to act as a session chair for the summer conference.  The dates of the conference are August 4-7, 1997 and the location is the Elkhorn Resort and Golf Club in Sun Valley, Idaho.  A tentative session title and schedule is listed below and is subject to change based on your evaluation of the abstracts in your session.  You may choose a more appropriate title for your session if you desire.

Enclosed you will find the abstracts that we have tentatively assigned to your session.  The address and other available information for the contact author (indicated by **) is also listed.

We are striving to improve the quality of the conference and are therefore asking that you review these abstracts for content, interest, originality, and above all quality.  If you feel that a paper does not meet standards please inform us that the paper should be rejected.  If a paper should be in another session tell us that also.  Also, consider the possibility of combining like papers by the same author if this is appropriate.  Otherwise, arrange the papers in the order that you feel appropriate with the intent of having 6 to 7 papers per session with a total of 25 minutes for each paper including 5 minutes for questions.  If a paper is a good one, it is acceptable to have 8 papers in a session � but no more than that.

Please return the enclosed sheet with the indicated information to us by March 31, 1997.   Faxing of the information will be good enough.  We will inform the authors as to acceptance or rejection of the papers.

Additionally, you will be asked to ensure that the authors in your session meet all deadlines for the abstract for publication and to see to it that they bring the required number of papers with them to the conference.  You should maintain contact with the authors periodically to see that they are on schedule.

Once again, thank you for your help and we look forward to a good conference this August.

AAS Technical Chair			AIAA Technical Chair
Felix Hoots					Bernard Kaufman
GRC International				Naval Research Laboratory
985 Space Center Drive, Suite 310		Code 8103
Colorado Springs, CO 80915			Washington, DC 20375
719/596-5395    719/596-6139 FAX		202/767-0513    202/404-7516 FAX
email: [email protected]			email:  HYPERLINK mailto:[email protected] [email protected]
ATTACHMENT 6
April 26, 1999

Dear Author:

	We are pleased to inform you that your paper has been accepted for presentation at the AAS/AIAA Astrodynamics Specialist Conference in Girdwood, Alaska to be held August 16-19, 1999.  Please note the following:

Please see the AAS website (  HYPERLINK mailto:[email protected] www.space-flight.org ) and check for the Girdwood conference to obtain complete author information including a preliminary program. Your assigned paper number will be listed in the preliminary program along with the name of your Session Chair. A set of instructions for the paper format, proceeedings submission/publication instructions, and a blank cover sheet will be available on the website May 1, 1999. Consider the site your primary source for author information.  

Each presenter will be scheduled for a total of 20 minutes (nominally a 15 minute presentation and 5 minute discussion).  Please keep in mind that the time schedule is fixed so that attendees may move between sessions.
You must bring 50 copies of your paper with you to the meeting.  Additionally, you must bring an original copy that will be used for the proceedings.  These preprints will be for sale in the paper room at the meeting.  In addition, a proceedings will be published after the meeting.  It is important that you bring these copies with you as there is a �No paper-No podium� rule that will be strictly followed.
Please note that publication in the proceedings is not considered an archival publication.  You are encouraged to submit your paper after the conference to one of the relevant journals such as:

Journal of the Astronautical Sciences
Kathleen Howell, Editor-in-Chief
School of Aeronautics and Astronautics
1282 Grisson Hall
Purdue University
West Lafayette, IN 47907
(765)494-5786;  (765)494-0307 FAX
[email protected]

Journal of Guidance, Control and Dynamics
George Schmidt, Editor-in-Chief
Mail Stop 57
The Charles Stark Draper Laboratory
555 Technology Square
Cambridge, MA 02139-3563
(617)258-3841; (617)258-2333
[email protected]


You must send  a 50 - 100 word abstract of your paper to both of the conference technical chairmen no later than 1 June.  This will be published in the conference program and will help attendees ascertain their interest in attending your presentation.  This should be sent by email as embedded text or as a WORD format attachment.  We will acknowledge our receipt of the abstract.  As with the requirement for the paper, this abstract is a necessity.

Finally, please send a biographical sketch to the Session Chair no later than 1 July for use in making introductions.  There will be a Speaker�s Breakfast each morning of the conference for all speakers presenting on that day.  It is requested that you attend this breakfast so that you can meet you Session Chair and coordinate any final presentation details.

We thank you for submitting this paper for consideration at the meeting, for your work involved in preparing the paper, presenting it, and sending the final version for the proceedings.  We look forward to your participation in the Astrodynamics Conference.


AAS Technical Chair				
Kathleen Howell
School of Aeronautics and Astronautics
GRIS 1282
Purdue University
West Lafayette, IN 47907
	765/494-5786  765/494-0307
email:[email protected]			

AIAA Technical Chair
Felix Hoots
GRC International
Suite 310
985 Space Center Drive
Colorado Springs, CO 80915
719/596-5395  719/596-6139
email: [email protected]			
ATTACHMENT 7

April 3, 1997

Dear Author:

	Your paper has been considered for presentation at the AAS/AIAA Astrodynamics Conference in Sun Valley, Idaho to be held August 4-7, 1997.  However, it has been determined that your paper is not appropriate for presentation at this conference for the following reason:

______  The subject matter is not consistent with the conference content.  We encourage you to consider submission to a more appropriate conference.

______  The content of your paper does not add significant new findings to the field of astrodynamics.  You may want to consider submitting it as an Engineering Note to an appropriate journal.

______  You have submitted a substantially similar version of your paper for another conference which will be held prior to this conference.  The call for papers clearly stated that only papers which have not been published or presented elsewhere would be considered.

______  You have previously submitted papers to our conference and have demonstrated a lack of common courtesy by failing to appear at the conference and giving us either no or very late notification of your withdrawal.

We thank you for submitting this paper for consideration at the meeting and for your interest in the conference..  We hope that you will consider our conference for presentation of your work in the future. 


AAS Technical Chair			AIAA Technical Chair
	Felix Hoots					Bernard Kaufman
	GRC International				Naval Research Laboratory
	985 Space Center Drive, Suite 310		Code 8103		
	Colorado Springs, CO 80915			Washington, DC 20375
719/596-5395    719/596-6139 FAX		202/767-0513    202/404-7516 FAX
email: [email protected]			email: [email protected]


ATTACHMENT 8

1999 ASTRODYNAMICS CONFERENCEAlyeska, AlaskaAug. 15-18, 1999SCHEDULE DATEEVENTRESPONSIBILITYMarch, 1998site selectionAAS GC&TCChairmenGC: AAS Kaufman        AIAA AlfriendTC:AAS Howell             AIAA HootsMar-98AIAA TC approval formGCMay-98draft call for papersTCJun-98finalize call for papersTCJun-98finalize hotel contractGCrequest reservation formsfor 2nd mailing in May 199810-Sep-98call for papers to AIAA-to appear in Nov. issueTCto AAS newsletter to appear in ****** issueOct-98selection of banquetGCNov-98initial budget preparation for Feb meetingGC/TCNov-98prepare material for first mailingGC/TC3-Dec-98first general mailingGCJan-99prepare final budgetGC/TCFeb-99presentation to committeesGCrequest session chairmenTC15-Feb-99Abstracts dueTC1-Mar-99tentative session scheduleTC1-Mar-99final date for decision to hotel on need for 4th dayGC/TC1-Mar-99Probable extension of abstract deadlineTC11-Mar-99selection of session chairmanTC11-Mar-99abstracts to session chairmanTC11-Mar-99arrangements with Jacobs for title page and GCauthor instructions25-Mar-99review by session chair for accept/rejectionTC5-Apr-99final programTC10-Apr-91acceptance letters/author instr./abstract formTCand hotel info10-Apr-99rejection lettersTC10-Apr-99cocktail party/cookout menu/final hotel detailsGC19-Apr-99arrangements for abstract bookletTC1-May-99final budgetGC13-May-992nd mailing to short list/reserv card/regist feeGC13-May-99abstract due to TCTC20-May-99abstracts to printerTC3-Jun-99program summary to authors/final remindersTC/session chairmen10-Jun-99final coordination /hotelGCtax exmpt status/billing procedurescocktail partyCookoutspeakers breakfastcommittee lunchesvisual equipment/microphonescheck on reservation status8-Jul-99arrangements with local bankGCcheck hotel reservation statusJuly **, 1999deadline for hotel
ATTACHMENT 9

Some authors, especially from foreign countries, may require a letter of invitation rather than our normal acceptance letter.  Additionally, they may request more information for visa applications or may request financial assistance.  The following example may meet their needs.
June 8, 1999
Ms. Qun Fang
College of Astronautics
Northwestern Polytechnical University
Xi(an 710072
P.R. China
Dear Ms. Fang:
On behalf of the program committee for the AAS/AIAA Astrodynamics Specialist Conference we are pleased to inform you that your paper, entitled Design and Analysis of Space Station Based Micro-Satellite Networks, has been accepted for presentation in the following session,
Session 2:	Formation Flying/Constellations
Day/Date:	Monday AM; August 16, 1999
Your paper has been assigned reference number AAS 99-313.  The reference number should be shown on correspondence and documents related to your paper.  Please be sure that your co-authors are informed of the acceptance of the paper.
This letter serves as the official invitation on behalf of the AAS and AIAA for yourself and co-authors to attend the 1999 Astrodynamics Specialist Conference in Girdwood, Alaska, U.S.A., August 16-19, 1999.  (Spouses are also welcome.)  It is not a commitment on the part of AAS or AIAA to provide any financial support.
Enclosed is a list of instructions for authors.  Please follow them carefully to insure that your paper meets the guidelines for papers to be presented at the conference.  Please note that you are encouraged to complete your travel arrangements soon.  If you or your co-authors are unable to present the paper, please inform us as soon as possible.
We look forward to receiving your paper and its presentation at the conference.
Sincerely,
Kathleen C. Howell	Felix Hoots
AAS Technical Chair	AIAA Technical Chair
School of Aeronautics and Astronautics	GRC International
GRIS 1282	Suite 310
Purdue University	985 Space Center Drive
West Lafayette, IN 47907	Colorado Springs, CO 80915
765/494-5786   765/494-0307	719/596-5395   719/596-6139
email:   HYPERLINK mailto:[email protected] [email protected]	email:   HYPERLINK mailto:[email protected] [email protected]
ATTACHMENT 10
Paper AAS 99-xxx


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Insert Paper Title Here

Insert Author Names Here

Insert Author Organization Here


AAS/AIAA Astrodynamics
Specialist Conference

Girdwood, Alaska		16-19 August 1999

AAS Publications Office, P.O. Box 28130, San Diego, CA  92129
ATTACHMENT 11

 EMBED Word.Picture.8    AAS/AIAA Astrodynamics SpecialistConference

Session 1, 8:30 � 11:30 AM		Session Title:		Mission Design: Mars
Session Chair:	Robert G. Melton

Architectural Design for a Mars Communications & Navigation Orbital 
Infrastructure 
0830am	R.J. Cesarone, R.C. Hastrup, D.J. Bell, D.T.Lyons, K.G. Nelson

Mars Network Constellation Design Drivers and Strategies: A Navigation Perspective
0850am	P. Kallemeyn, T. Ely, J. Guinn, M. Jah, Y. E. Bar-Sever, S. Lichten, S-C. Wu, L. Romans, D. Bell, E. Levene

Mars Polar Lander Entry Descent & Landing Design 
0910am	W. H. Willcockson

The Strategy for the Second Phase of Aerobraking Mars Global Surveyor
0930am	M.D. Johnston, P.B. Esposito, V. Alwar, S.W. Demcak, E.J. Graat, P.D. Burkhart, B.M. Portock

Aladdin's Phasing and Mission Orbit Design
1010am	Y. Guo 

Mission Design Overview for the 2003/2005 Mars Sample Return Mission
1030am	L. A. D'Amario, R. B. Roncoli, J. C. Smith

Mars Orbit Rendevous Strategy for the Mars 2003/2005 Sample Return Mission
1050am	L. A. D'Amario, W. E. Bollman, W. J. Lee, R. B. Roncoli, J. C. Smith

Terminal Rendezvous Analysis and Design for the Mars Sample Return Mission
1110am	P. S. Kachmar, C. N. D'Souza, T. J. Brand

ATTACHMENT 12

Dear Session Chairs,

We are looking forward to seeing everyone at the AAS/AIAA Astrodynamics Specialist Conference in Girdwood, Alaska, August 16-19, 1999.

This is just a reminder to contact all the authors in your session and remind them of the following:

The authors are reminded that all paper instructions are on the AAS web site. A new cover page is also on the site with the new AAS logo.

The authors must bring 50 copies of their paper to the meeting.  Additionally, they must bring an original camera ready copy that will be used for the proceedings.

The final version of the program is now available on the AAS web site. This version includes  paper numbers and session assignments as well as short abstracts for the papers as well as the conference schedule and activities.

This is the last chance for authors to inform us if they require a 35 mm slide projector or VCR for their presentation. It will not be possible to accommodate last minute requests.

The authors should provide a short biography to their session chairs.

It is extremely important that you provide this information to your session authors.  We will not be sending this message to them separately.   Forwarding this information is your responsibility as the session chair.  If you have any other questions or concerns, please let us know.


AAS Technical Chair				
Kathleen Howell
School of Aeronautics and Astronautics
GRIS 1282
Purdue University
West Lafayette, IN 47907
	765/494-5786  765/494-0307
email:[email protected]			

AIAA Technical Chair
Felix Hoots
GRC International
Suite 310
985 Space Center Drive
Colorado Springs, CO 80915
719/596-5395  719/596-6139
email: [email protected]	
ATTACHMENT 13

Instructions for the Use of the Personal AAS/AIAA Conference Planner

For the Conference Chairmen:
The planner lists typical events at an AAS sponsored conference.  This includes speaker�s briefings, coffee breaks, technical committee meetings and receptions.  It is intended to allow a conference attendee to organize which papers and events he/she plans on attending. 
For each day, the following columns are provided:
Time of Day -- To be filled in by the conference chairmen.  Note, in some past conferences, papers have been scheduled simultaneously with committee meetings. 
A personal use column with a  "  at the top.  The column should be reserved for personal use.  The conference attendee can use this column to indicate if they attended the paper, or if they purchased the paper, or for any other use.
Session ID -- To be left blank.
Room -- To be filled in by the conference chairmen for known events, otherwise to be left blank.  The sample sheet has room names filled in for some of the events from the January 2000 AAS/AIAA Space Flight Mechanics Meeting in Clearwater, FL.  These, obviously, will have to be changed.
Activity/Paper � Known activities should be filled in by the conference chairmen but should not span the entire column, so as to allow the user to write in their personal plans.  (For example, not everyone attends the technical committee meeting.)  The remaining rows should be left blank for personal use.

PAGE  


PAGE  1


PAGE  1


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ALASKA COSTS

Description

cost

updated

comments

Actual Cost

Comments

Pre-conf. cost

mailings

$1,318

x

$.32 each-twice, 200 for foreign+350 for AIAA

$350.00

aiaa

$146

x

150 authors-twice, 50 for foreign

Misc

$2,200

x

200 misc., 2000 student award

program printing

$1,500

x

estimate from Terry was around $1000

total pre-conf

$5,164

$350.00

location costs-food

speakers brkfst

$1,752

x

$9/person 3 days; 55people/3days

all food prices have 18% added

coffee breaks

$2,832

x

$2/person; 2 per day

this is already included in the estimate

morning danish

$0

committee lunch

$1,133

x

2 @$16/person

reception

bar

$0

unknown for 2 receptions and dinner

early registration

$5,098

x

200 people

food and two drinks

2nd reception

$9,487

x

300 people

food and two drinks

cookout

open bar

$0

unknown

food

$4,257

x

150 people cost to each $20; sub is 16.58+11.80 for 2 drinks

dinner is $48.38/person; sub by $28.38

misc

$1,550

bar tenders ($1000),550 for Glacier Express

must check with hotel

total food

$26,109

<---Includes 18% gratuity

$0

location-other

eqt. rental

$705

x

3 overhead/3 days; one vcr and one 35mm

helpers

$300

x

this is for registration desk and paper sales

room rental

$2,350

x

spkr transportation

$0

misc

$500

x

total location other

$3,855

$0

TOTALS

Differences

pre-conf

$5,164

$350.00

location-food

$26,109

$0.00

location-other

$3,855

$0.00

total cost

$35,128

$350.00

$0.00

total cost+margin

$40,397

<----margin of 15%                               no margin ---->

$350.00

less sales of papers

$2,000

Total final cost

$38,397

registration fee

$192

based on 200 people all members

members**

$190

150 M

$190--member, $240-nonmember, $25-student

non members**

$240

50 nm

based on 150 members, 50 non-members, 15 students

students**

$25

15 s

$40,875



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1999 ASTRODYNAMICS CONFERENCE

Alyeska, Alaska

Aug. 15-18, 1999

SCHEDULE DATE

EVENT

RESPONSIBILITY

COMMENTS

March, 1998

site selection

AAS GC&TC

completed

chairmen

GC: AAS Kaufman

completed

        AIAA Alfriend

TC:AAS Hoots

             AIAA Howell

Mar-98

AIAA TC approval form

kaufman

May-98

draft call for papers

TC

Jun-98

finalize call for papers

TC

Jun-98

finalize hotel contract

kaufman

request reservation forms

for 2nd mailing in May 1998

10-Sep-98

call for papers to AIAA-to appear in Nov. issue

TC

to AAS newsletter to appear in ****** issue

Oct-98

selection of banquet

GC

Nov-98

initial budget preparation for Feb meeting

GC/TC

Nov-98

prepare material for first mailing

GC/TC

3-Dec-98

first general mailing

GC/kaufman

Jan-99

prepare final budget

GC/TC

Feb-99

presentation to committees

GC

request session chairmen

15-Feb-99

Abstracts due

TA/RD

1-Mar-99

tentative session schedule

TC

1-Mar-99

final date for decision to hotel on need for 4th day

GC/TC

This is important

11-Mar-99

selection of session chairman

TC

11-Mar-99

abstracts to session chairman

TC

11-Mar-99

arrangements with Jacobs for title page and 

GC

author instructions

25-Mar-99

review by session chair for accept/rejection

5-Apr-99

final program

TC

10-Apr-91

acceptance letters/author instr./abstract form

TC

and hotel info

10-Apr-99

rejection letters

TC

10-Apr-99

cocktail party/cookout menu/final hotel details

GC/kaufman

19-Apr-99

arrangements for abstract booklet

TC

1-May-99

final budget

GC

13-May-99

2nd mailing to short list/reserv card/regist fee

GC

13-May-99

abstract due to TC

TC

20-May-99

abstracts to printer

TC

3-Jun-99

program summary to authors/final reminders

TC/session chairmen

10-Jun-99

final coordination /hotel

GC

tax exmpt status/billing procedures

cocktail party

cookout

speakers breakfast

committee lunches

visual equipment/microphones

check on reservation status

8-Jul-99

arrangements with local bank

GC

check hotel reservation status

July **, 1999

deadline for hotel



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Zhang) Dept of Power, Inner Mongolia Technology University, Huheha�(Banerjee) Consulting Scientist, H1-61/250, Lockheed Martin ATC, Palo Alto, CA 94304, Phone: 650-424-2624, Fax: 650-424-3106, [email protected] (Singhose) Mechanical Engineering Dept, Georgia Institute of Technology, Atlanta, GA 30332, Voice: 650-424�Misra, Arun K.                       Sedlak, Joseph                                Gregory, Jim; Jones, Sonny                                      Smilek, Ron ; Lorentz, Dave                                         Bowser, Robert; Mylod, Pat              �(Martinot) Departement Missions et Performances des Systemes, Service Performances Operationnelles, Voice: 05-34-35-65-16, Fax: 05-34-35-61-63, [email protected] (Vignaux) Voice: +33-5-6119-4508, Fax: +33-5-6119-6163, david.vignaux.alcatel�George Washington Univ, Joint Institute for the Advancement of Flight Sciences, Langley Research Center, MS 269, Hampton, VA 23681-2199, Voice: 804-864-1982, Fax: 804-864-5894, [email protected], (Home) 7505 River Road, Apt. PE, Newport News, VA 236�(Oshman) Dept of Aerospace Engineering, Technion - Israel Institute of Technology, Haifa 32000, Israel, Voice: +972-4-829-3803, Fax: +972-823-1848, [email protected] (Dellus) MBT Systems and Space Technology, Electronic Division, Israeli Aircraft I�(Chodas) Jet Propulsion Lab, California Institute of Technology, 4800 Oak Grove Dr, MS 301-150G, Pasadena, CA 91109-8099, Voice: 818-354-7795, Fax: 818-393-1159, [email protected] (Yeomans) Voice: 818-354-2127, Fax: 818-393-1159, donald.yeomans@jpl�(Kawaguchi) The Institute of Space and Astronautical Science, 3-1-1 Yoshinodai, Sagamihara, 229-8510, Japan, Voice: +81-42-759-8219, Fax: +81-42-759-8458, [email protected] (Yoshikawa) Advanced Technology R&D Center, Mitsubishi Electric Co., 8-1-1 �(Jesus) Universidade Estadual de Feira de Santana-UEFS, Feira de Santana, BA, Brasil, Voice/Fax: 55-75-2248-85; [email protected] (Souze, Prado) Instituto Nacional de Pesquisas Espaciais-S.Jose dos Campos, SF, 12227-010, Voice: 55-12-3456201, Fax: 55-12-3456226�(Robertson, Singhose) Dept of Mechanical Engineering, Georgia Institute of Technology, Atlanta, GA 30332, Voice: 404-385-0668, Fax: 404-899-9342, [email protected] (Singhose) Voice: 404-385-0668, Fax: 404-894-9342, [email protected] (Bane�Antreasian, P.G.                              Helfrich, C.L.                                     Miller, J.K.; Owen, W.M.                                       Williams, B.G.                                   Yeomans, D.K.                                 �(Antreasian, Helfrich, Miller, Owen, Williams, Yeomans, Giorgini) Jet Propulsion Lab, California Institute of Technology, 4800 Oak Grove Dr, Pasadena, CA 91109-8099, Voice: 818-354-4381, Fax: 818-393-5214, [email protected] (Scheeres) Dept of Aerospace�(Mortari/Castronuovo) Universita' degli Studi "La Sapienza" di Roma, Via Salaria, 851 - 00138 Roma, Italy, Voice: +39(06)812-0529, Fax: +39(06)810-5241, [email protected], [email protected] (Barsocchi) Via Cimabue, 7, 00034 �(Mortari/Angelucci) Universita' degli Studi "La Sapienza" di Roma, Via Salaria, 851 - 00138 Roma, Italy, Voice: +39(06)812-0529, Fax: +39(06)810-5241, [email protected] (Junkins) Texas A&M Univ, 722 Bright Blvd., College Station, TX 77843-3�(Mortari/Angelucci) Universita' degli Studi "La Sapienza" di Roma, Via Salaria, 851 - 00138 Roma, Italy, Voice: +39(06)812-0529, Fax: +39(06)810-5241, [email protected] (Gigli) Alenia Difesa, Divisione Sistemi Avionici ed Equipaggiamenti Un�Helfrich, C.E.                                     Miller, J.K.                                           Antreasian                           Carranza, E.                                       Williams, B.G.                                        Dunham,�(Helfrich, Miller, Antreasian, Carranza, Williams) Jet Propulsion Lab, California Institute of Technology, M/S 301-150, 4800 Oak Grove Dr, Pasadena, CA 91109-8099, Voice: 818-354-1446, Fax: 818-393-6388, [email protected] (Dunham, Farquhar, McAd�Kallemeyn, Pieter                            Cangahuala, Alberto                      Ely, Todd; Bell, David                                            Guinn, Joseph                                   Bar-Sever, Yoaz E.                         Lichten, Ste�(Longman) Columbia Univ, MS 4703, Rm 220, Mudd Bldg, 500 West 120th St, NY, NY 10027, Voice: 212-854-2959, Secretary#: 212-854-2965, [email protected] (Giese) Swiss Federal Institute of Technology Zurich (ETH), Zurich, Switzerland (Bock) Univ of Heidelber�Jet Propulsion Lab, California Institute of Technology, 4800 Oak Grove Dr, MS 301-276, Pasadena, CA 91109, Voice: 818-354-3209, Fax: 818-393-5214, [email protected], [email protected], [email protected], [email protected]�(Weeks) Loyola Marymount Univ, 7900 Loyola Blvd, LAX, CA 90045-8130, Voice: 310-338-5108, Fax: 310-338-7339, [email protected] (Miller) Jet Propulsion Lab, California Institute of Technology, MS 301/125j, 4800 Oak Grove Dr, Pasadena,  CA 91109, Voice�(Bir) Air Force Research Lab/VSSS, 3550 Aberdeen Ave SE, Kirtland AFB, NM 87117-5718, Voice: 505-853-4136, Fax: 505-846-6053, [email protected] (Carter) Voice: 505-853-3970, Fax: 505-846-0033, [email protected] (Sabol) Voice: 505-846-4056, Fax: 50�(Carter) Air Force Research Lab/VSSS, 3550 Aberdeen Ave SE, Kirtland AFB, NM 87117-5718, Voice: 505-853-3970, Fax: 505-846-0033, [email protected] (McLaughlin) Voice: 505-853-6545, Fax: 505-846-6053, [email protected] (Sabol) Voice: 505-846-4056, Fax: �(Carter) Air Force Research Lab/VSSS, 3550 Aberdeen Ave, SE, Kirtland AFB, NM 87117-5718, Voice: 505-853-3970, Fax: 505-846-0033, [email protected] (Sabol) Voice: 505-846-4056, Fax: 505-846-6053, [email protected] (Burns) Voice: 505-846-2352, Fax: 505-84�(Harvie) ASRC Aerospace, 6411 Ivy Ln, #610, Greenbelt, MD 20770, Voice: 301-345-4500 X229, Fax: 301-345-9274, [email protected] (Phenneger) X231, [email protected] (Dress) NOAA, Dept of Commerce, FOB#4, Suitland, MD 20746, Voice: 301-457-5�Lemoine, F.G.                                   Rowlands, D.D.                                 Smith, D.E.; Pavlia, D.E.                                 Chinn, D.S.; Luthcke, S.B.                                            Neumann, G.A.                   �(Lemoine, Rowlands, Smith) Lab for Terrestrial Physics, NASA Goddard Space Flight Center, Code 926, Greenbe<  lt, MD 20771, Voice: 301-614-6109, Fax: 310-614-6099, [email protected] (Pavlia, Chinn, Luthcke) Raytheon ITSS, Greenbelt, MD (Neumann, Zu�(Dress) NOAA, Dept of Commerce, FOB#4, Suitland, MD 20746, Voice: 301-457-5180 X196, Fax: 301-457-5175, [email protected] (Harvie) ASRC Aerospace, 6411 Ivy Ln, #610, Greenbelt, MD 20770, Voice: 301-345-4500 X229, Fax: 301-345-9274, edwin.harvie@akspa�(Beckman) Goddard Space Flight Center, Code 572, Greenbelt, MD 20771, Voice: 301-286-8866, Fax: 301-286-0369, [email protected] (Guzman) Purdue Univ, Grissom Hall 1282, West Lafayette, IN 47907-1282, Voice: 765-494-5132, Fax: 765-494-0307, jguzma�(Jean) Universite de Sherbrooke, 2500, boul de l'Universite, Sherbrooke, (Quebec), J1K 2R1, Canada, [email protected] (Pierrik) ESA/ESTEC, Keplerlaan 1, 2201 AZ Noordwijk, the Netherlands (Pieter) Verhaert Design and Development nv, Hogenakk/A Technique for Earth Escape Using a Solar Sail`D'Souza, Christopher N.              Kachmar, Peter S.                         Brand, Timothy J.JTerminal Rendezvous Analysis and Design for the Mars Sample Return MissionN/A>Hoots, Felix R.                             France, Richard G.&Satellite Drag Error Growth EstimationNo.Rec'dAuthorTitle	Addresses	File NameArea of InterestOAAS99_abs.doc;                                                 odea.ps; odee.psXAlaska abstract cover letter1.doc;                                   Alaska Abstract.doc4Navigation Strategy for the Mars 2001 Lander MissionAbstract_Submission.pdf?Ong, Kwok M., Dr.                               Kamel, Ahmed A.Shaping.docOReducing Conservatism of Analytic Transient Response Bounds via Shaping Filters�Misra, Arun K.                                              Min, B.                                                     Cyril, X.                                            Modi, V.J.                                                deSilva, C.W.�Modi, V.J.                                                 Cao, Y.                                             deSilva, C.W.                               Misra, A.K.                                   dCicci, David A, Dr.                   Lovell, T.A.                                        Qualls, C.?Chern, Jeng-Shing                               Sheu, Dong-Long7Deviating an Earth-Pointing Asteroid under Lunar Effect�(Chern) Chung Shan Institute of Science and Technology, POB 90008-6-7, Lungtan, Taiwan 32526, R.O.C., [email protected] (Sheu) IAA, National Cheng Kung Univ, Tainan, Taiwan 70101, R.O.C.	AAS01.doc^Wilson, R.S.                                 Howell, Kathleen C.                      Lo, M.W.ROptimization of Insertion Cost for Transfer Trajectories to Libration Point Orbits(ATTDES - Generalized Equations of Motion|Univ of Colorado, Campus Box 429, Boulder, CO 80309-0429, Voice: 303-492-6417, Fax: 303-492-7881, [email protected]astro99-abstract.docAttitude Control, ToolsbJu, Gwanghyoek                                Pollack, Tom                        Junkins, John L.WDIGISTAR II Micro-Star Tracker: Autonomous On-Orbit Calibration and Attitude Estimation(Alaska99Abstract.doc; Alaska99Letter.doc�Texas A&M Univ, College Station, TX, Voice: 409-845-0720 (Home) 2500 Central Park Ln #2105, College Station, TX 77840, [email protected]Willcockson, William H.0Mars Polar Lander Entry Descent & Landing Design5AIAAAbstractSubmittal.MW.doc; MSPEDLPaperAbstract.doc�Lockheed Martin Astronautics, S8800, POB 179, Denver, CO 80201, Voice: 303-977-5094, Fax: 303-977-9345, [email protected];Oshman, Y.                                       Dellus, F.WSpacecraft Angular Velocity Estimation Using Sequential Observations of a Single Vectorasc99.pdf; asc99.psRaman, Kidambi V.?Multiple Approaches for GYRO Calibration of INTELSAT Satellitesdcalabs.docPalmerini, Giovanni B.,Guidance Strategies for Satellite Formations�Scuola di Ingegneria Aerospaziale, Universita degli Studi di Roma "la Sapienza" 18, via Eudossiana - 00184 Roma - Italy, Voice: +39.06.44585.334, Fax: +39.06.44585.952, [email protected]Human, Mel :Generalized Planetary Reentry Minimal Heating Trajectories>Chodas, Paul W.                             Yeomans, Donald K.VPredicting Close Approaches and Estimating Impact Probabilities for Near-Earth Objects	Ast99.doc8Attitude Dynamics and Control: Applications - Chris HallCombine with # 152Combine with #147Rejected by Session ChairIA Study of the Deployment Dynamics of the ASTOR Tethered Satellite SystemAbstract for Alaska.docSnow, Daniel*Element Set Prediction Accuracy Assessment [email protected]
ABSTRACT1.doc?Eke, F.O.                                             Eke, E.M.OEffects of Internal Mass Flow on the Attitude Dynamics of Variable Mass SystemsAas=AIAAabstract-99.docWConstellation Design for a Mars-Orbiting Satellite Communication and Navigation Network^Jet Propulsion Lab, Voice: 818-354-9166, Fax: 818-393-6388, [email protected]MarsNet Abstract.doceGranholm, George R.                     Proulx, Ronald J.                             Cefola, Paul J.?Methods of Orbit Determination for EllipsoTM Sub-Constellations*,�The Charles Stark Draper Lab, MS 70, 555 Technology Square, Cambridge, MA 02139, Voice: 617-258-1559, Fax: 617-565-8674, [email protected]
ala abstr.docEThe Strategy for the Second Phase of Aerobraking Mars Global SurveyorMGS-AB2-mdj.docRoss, I, Michael,Thrust Programming in Aeroassisted ManeuversRoss Pap.pdfMatousek, SteveESpaceTime - A MIDEX Proposal to Test Einstein's Equivalence Principle�Jet Propulsion Lab, California Institute of Technology, MS 264-426, 4800 Oak Grove Dr, Pasadena, CA 91109, Voice: 818-354-6689, Fax: 818-393-6800, [email protected]Aug 99 AK abs-Matousek.pdf�Lee, Wayne J.                                    D'Amario, Louis A.                        Roncoli, Ralph B.                            Smith, John C.@Mission Design Overview for Mars 2003/2005 Sample Return Mission-aas99 msr abstract.doc aas99 msr abstract.pdfAHack, Kurt J.                                      Riehl, John P.GTrajectory Development and Optimization of an RBCC-based Launch VehiclepHarsch, Jenna                                  Middour, Jay                                     Llewellyn, Robinabs.psTSpaceflight Dynamics Support for the MightySat II.1 Hyperspectral Payload Operations�Carter, Scott Capt.                         Sabol, Chris Dr.                                Burns, Richard                                 Bir, Megan Lt./A Fresh Look at Angles-Only Orbit DeterminationDesai, Prasun N. HEntry Dispersion Analysis for the Muses-C Asteroid Sample Return CapsulePark, Sang-YounghThermally-Induced Attitude Vibration Control of a Spacecraft with a Flexible Boom Using Smart StructuresMNavigating Mars Global Surveyor through the Martian Atmosphere: Aerobraking 2RControl Methods for the Activation and Operation of the GOES On-Orbit Storage ModeEStorage Control Abstract(1).doc;      Storage Control Abstract(1).txtcDress, Andre                               Harvie, Edwin                            Phenneger, Milt)Relative Equilibria of Orbiting Gyrostats<Hall, Christopher D.                        Beck, Jeffrey A.;System Design Considerations for a Formosa-X Microsatellite	AAS02.docChern, Jeng-ShingtChung Shan Institute of Science and Technology, POB 90008-6-7, Lungtan, Taiwan 32526, R.O.C., [email protected]Penzo, Paul A.8Venus and Beyond Using the Ariane ASAP Launch Capability�Jet Propulsion Lab, California Institute of Technology, MS 301-140H, 4800 Oak Grove Dr, Pasadena, CA 91109, Voice: 626-354-6162, Fax: 626-393-9900, [email protected]Sauer, Carl G., Jr.?Solar Sail Trajectories for Solar Polar and Heliopause Missions�Jet Propulsion Lab, California Institute of Technology, MS 301-140H, 4800 Oak Grove Dr, Pasadena, CA 91109, Voice: 818-354-4875, Fax: 818-393-9900, [email protected]�(Hall) Virg<  inia Polytechnic Institute & State Univ, Blacksburg, VA 24061, Voice: 540-231-2314, Fax: 540-231-9632, [email protected] (Beck) Air Force Research Lab, Kirtland AFB, NM 87117Sess 17fThe Aerospace Corp, POB 92957, M4/947, LAX, CA 90009-2957, Voice: 310-336-4307, [email protected]�Lockheed Martin Missiles & Space, O:L8-30 (E5-10) 8:102, 1111 Lockheed-Martin Way, Sunnyvale, CA  94089, Voice: 408-756-3973, Fax: 408-743-0699, [email protected]�Jet Propulsion Lab, California Institute of Technology, MS 301-150, 4800 Oak Grove Dr, Pasadena, CA 91109-8099, Voice: 818-354-7201, Fax: 818-393-6388, [email protected]�Jet Propulsion Lab, California Institute of Technology, MS 301-142, 4800 Oak Grove Dr, Pasadena, CA 91109-8099, Voice:  818-354-0313, Fax: 818-393-9900, [email protected]�Univ of California, 38-137 Engineering IV, POB 951597, 420 Westwood Plaza, Box 951597, LAX, CA 90095-1597, Voice: 310-825-2902, Fax: 310-236-2302, [email protected]"This was a duplicate - leave blankXPourtakdoust, S.H.                        Mehri B.                    Novinzadch, A.R.B.uAn Investigation of Satellite Oscillations in an Arbitrary Orbit Using Regular Perturbation Theory and the WKB Method]Sharif Univ of Technology, Dept of Mech Eng, Fax: 98-21-918-23-66, [email protected]?Mitchell, Jason Wm.A Simplified Variation of Parameters Formulation of Euler's Equations of Motion of an Arbitrarily Torqued Asymmetric Rigid Body�Univ of Cincinnati, Dept of Aeospace Eng & Eng Mechanics, ML70, Cincinnati, OH 45221-0070, Voice: 513-556-6499 Fax: 513-556-5038, [email protected]�Lo, Martin W.                       Koon, Wang Sang                           Ross, Shane                       Marsden, Jerrold                    .The Genesis Trajectory and Heteroclinic Cycles]Jet Propulsion Lab, California Institute of Technology, 4800 Oak Grove Dr, Pasadena, CA 91109<Ricci, Mario Cesar                     Varotto, Sebastiao C.5Development of a Bapta Mechanism for Small SatelliteswSAIC, 1501 Woodfield Rd, #202N, Schaumburg, IL  60173, Voice: 847-330-2524, Fax: 847-330-2522, [email protected]�Analytical Graphics, Inc, Voice: 610-578-1095, [email protected] (Home) POB 647, Morgantown, PA 19543, Voice: 610-286-1795, Fax: 610-286-4798�(Nicholas) Naval Research Lab, Code 7623, 4555 Overlook Ave, Washington, DC 20375, Voice: 202-767-2441, Fax: 202-767-9388, [email protected] (Thonnardj) Code 7623 (Picone) Code 7643�Jet Propulsion Lab, California Institute of Technology, 4800 Oak Grove Drive, MS 301-125L, Pasadena, CA 91109-8099, Voice: 818-393-1744, Fax: 818-393-6388, [email protected]�Jet Propulsion Lab, Navigation and Flight Mechanics Section, California Institute of Technology, 4800, Oak Grove Drive, Pasadena, CA 91109-8099, Voice: 818-354-8132, Fax: 818-393-6388, [email protected]�Space Systems/Loral, 3825 Fabian Way, M/S G76, Palo Alto, CA 94303-4604, Voice: 650-852-4210, Fax: 650-852-4928, [email protected]AUGUST 1999 - AAS/AIAA ASTRODYNAMICS CONFERENCE - ALASKATurner, Andrew E.
Yan, Hui, Dr.Haley, David R.rAntonio Fernando Bertachini de Almeida Prado; Maria Matilde Netto dos Santos Paulo; Marcelo Lopes Oliveira e SouzaUnsuccessful e-mail2Pardini, C.                            Anselmo, L. 2Guelman, Mauricio                        Tahan, D.[Solar Electric Propulsion Earth to Mercury Optimal Trajectories with Variable Maximum PowerSchaechter, David3A Fully-Redundant Set of Single-Axis AccelerometersKechichian, Jean A.V(Owens) NASA MSFC (Vaughan) Univ of Alabama, Huntsville, AL, [email protected]AFRL, [email protected]Naval Research Lab, Washington, DC  20375, [email protected][The Charles Stark Draper Lab, 555 Technology Square, Cambridge, MA 02139, [email protected]Neutral Atmosphere Density Monitoring Based on Space Surveillance System Orbital Data�(Wilson & Lo) Jet Propulsion Lab, California Institute of Technology, 4800 Oak Grove Dr, Pasadena, CA 91109-8099 (Howell) School of Aeronautics & Astronautics, Purdue Univ, 1282 Grissom Hall, West Lafayette, IN  47907-1282�ITT Industries, 4450 E. Fountain Blvd, Colorado Springs, CO 80916 (Walker) Voice: 719-637-5938, Fax: 719-637-5960, [email protected] (Casali) Voice: 719-591-3663, Fax: 719-637-5960, [email protected] xAnalytical Graphics, Inc, 325 Technology Dr, Malvern, PA 19355, Voice: 610-578-1030, Fax: 610-578-1001, [email protected]Wnuk, Edwin\Relation between Osculating and Mean Orbital Elements in the Case of the Second Order Theory�Astronomical Observatory of the A. Mickiewicz Univ, ul.Sloneczna 36, PL-60-286 Poznan, Poland, Voice/Fax: +48(61)8686511, [email protected]Viereck, Rodney'Solar Maximum Effects on Satellite Drag'NOAA Space Environment Lab, Boulder, CO=Owens, J.                                       Vaughan, W.W..Solar predictions for Space Station OperationscNicholas, A.C.                             Picone, J.M.                              Thonnard, S.E.rA Methodology for Using Optimal MSIS Parameters Retrieved from SSULI Data to Compute Satellite Drag on LEO Objects0Marcos, F.A.                               et al@Operational Application of the Atmospheric Calibration TechniqueMinnow, Joe Dr.Sverdup, Inc., Huntsville, ALaTBD - Interested in contributing a paper; likely topic is potential upgrades to empirical models.4Special Session: Atmospheric Modeling - Frank Marcos&Mission Design: Planets - Lou D'Amario%Trajectory Optimization - John HansonTethers - Arun Misra"Prediction/Uncertainty - Beny Neta"Attitude Estimation - Don Mackison(Guidance and Navigation - Bobby Williams Orbit Dynamics - Paul Schumacher Attitude Dynamics - John CochranIMission Design: Near Earth, Earth/Moon, and Libration Points - Dave FoltaAAS #Actions�Jet Propulsion Lab, California Institute of Technology, MS 264-380, 4800 Oak Grove Dr, Pasadena, CA 91109, Voice: 818-354-8784, Fax: 818-393-2902, [email protected]This is a duplicate of # 7�Jet Propulsion Lab, California Institute of Technology, 4800 Oak Grove Dr, M/S 264-235, Pasadena, CA 91109, Voice: 818-393-1290, Fax: 818-393-3147, [email protected]�Naval Postgraduate School, 699 Dyer Rd, Rm 137, Monterey, CA 93943-5000, Voice: 831-656-2074, Fax: 831-656-2313, [email protected]�(Hack) NASA, John Glenn Research Center at Lewis Field, 2100 Brookpark Rd, MS 500-201, Cleveland, OH, Voice: 216-977-7060, Fax: 216-977-7125, [email protected] (Riehl) Voice: -7061, [email protected]~U.S. Naval Research Lab, 4555 Overlook Ave SW, Washington DC, Voice: 202-767-6509, Fax: 202-404-7516, [email protected]�The Johns Hopkins Univ, APL, Rm 4-141, 11100 Johns Hopkins Rd, Laurel, MD 20723-6099, Voice: 240-228-7541/443-778-7541, Fax: 240-228-1093/443-778-1093, [email protected]}Texas A&M Univ, H.R. Bright Bldg, Rm 701, College Station, TX, Voice: 409-845-5920, Fax: 409-845-6051, [email protected]�Columbia Univ, MS 4703, Rm 220, Mudd Bldg, 500 West 120th St, New York, NY 10027, Voice: 212-854-2959, Secretary#: 212-854-2965, [email protected]�The Univ of Texas at Austin, 3925 W. Braker Ln, #200, Austin, TX 78759-5321, Voice: 512-471-7175, Fax: 512-471-3585, [email protected]�Jet Propulsion Lab, 4800 Oak Grove Dr, California Institute of Technology, Pasadena,  CA 91109, Voice: 818-354-5093, [email protected]�(Herman) Spectrum Astro, Inc, 1440 North Fiesta Blvd., Gilbert, AZ 85233, Voice: 602-892-8200, Fax: 602-892-2949, [email protected] (Spencer) Air Force Research Laboratory/VSSS, Kirtland AFB, NM 87117-5776, [email protected] �Jet Propulsion Lab, 4800 Oak Grove Dr, California Institute of Technology, MS 301-125J,  Pasadena, CA, Voice: 818-354-3606, [email protected]{The Aerospace Corp, POB 92957, M4/962, LAX, CA 90009-2957, Voice: 310-336-5572, Fax: 310-336-1812, [email protected]�Jet Propulsion Lab, California Institute of Technology, Pasadena,  CA 91109, Voice: 818-393-1004, Fax: 818-393-3147 daniel.t.lyon<  [email protected]Analytical Grahpics, Inc, 325 Technology Dr, Malvern, PA 19335, Voice: 610-578-1000, Fax: 610-578-1001, [email protected]�The Aerospace Corp, POB 92957, M4/946, LAX, CA 90009-2957, Voice: 310-336-4297, Fax: 310-336-5827, [email protected] (Oltrogge) Voice: 719-554-6026, Fax: 719-554-5876, [email protected]=NASA Langley Research Center, MS 365, Hampton, VA 23681-2199 vNaval Postgraduate School, 699 Dyer Rd, Bldg 245, Monterey, CA 93943-5000, Voice: 408-656-2656, [email protected]�Jet Propulsion Lab, California Institute of Technology, 4800 Oak Grove Dr, Pasadena, CA 91109, Voice: 818-393-1264, Fax: 818-393-3147, [email protected]Jet Propulsion Lab, California Institute of Technology, 4800 Oak Grove Dr, Pasadena, CA 91109, [email protected]Jet Propulsion Lab, California Institute of Technology, 4800 Oak Grove Dr, Pasadena, CA 91109, [email protected]�The Pennsylvania State Univ, 227 Hammond Bldg, Univ Park, PA 16802-1401, Voice: 814-865-4523, Fax: 814-863-7967, [email protected]Receipt          E-mailed�Johnston, M.D.                               Esposito, P.B.                                  Alwar, V.; Demcak, S.W.                                   Graat, E.J.; Burkhart, P.D.                                   Portock, B.M. �(Demarest) Univ of Texas at Austin, 3925 W. Braker Ln, #200, Austin, TX 78759-5321, Voice: 512-471-5509, Fax: 512-471-3570, [email protected] (Schutz) Voice: 512-471-4267, Fax: Same, [email protected]de Lafontaine, Jean               Vuilleumier, Pierrik                 Van den Braembussche, Pieter*Autonomous Control of the Proba SpacecraftAAS AIAA Astrod Conf.doc�(Longman) Columbia Univ, MS 4703, Rm 220, Mudd Bldg, 500 West 120th St, NY, NY 10027, Voice: 212-854-2959, Secretary#: 212-854-2965, [email protected] (Plotnik) Allied Signals, Inc, Teterboro, NJ�Esposito, P.B.; Alwar, V.                                               Burkhart, P.D.; Demcak, S.W.                                   Graat, E.J.; Johnston, M.                                                       Portock, B.M. 4Howell, K.C.                            Barden, B.T.1Formation Flying Near the Sun-Earth/Moon L1 Point)*
+�Purdue Univ, 1282 Grissom Hall, West Lafayette, IN 47907-1282 (Howell) Voice: 765-494-5786, Fax: 765-494-0307, [email protected] (Barden) Voice: 765-494-5813, Fax: Same, [email protected]ICESat Attitude Algorithm for Maintained Reference Groundtrack Pointing�Kubitschek, Daniel G.              Gold, Kenneth                         Ondrey, Michael                      Axelrad, Penina                        Born, George H.�Univ of Colorado, Campus Box 431, Boulder, CO 80309-0431, Voice: 303-492-6677, Fax: 303-492-2825, [email protected]Orbit Analysis Tools Software (Version 1 for WindowsTM)46�Cochran, J.E. Jr.                                   Cho, S.                                    Lovell, A.                                     Cicci, D.A.IModeling Tethered Satellite Systems for Detection and Orbit DeterminationeAuburn Univ, 211 Aerospace Engineering Bldg, Auburn, AL 36849, Voice: 334-844-4874, Fax: 334-844-6803<Demarest, P.                                    Schutz, B.E.3Maintenance of the ICESat Exact Repeat Ground TrackGuo, Yanping*Aladdin's Phasing and Mission Orbit DesignAAS Aug abs.doc=Alfriend, Kyle T.                                Paik, SokwonUCovariance as an Estimator of Orbit Prediction Error Growth for Geosynchronous OrbitsGEO Study Abstract.docBiases-Abstract.docAnchorage-Abstract.docDAlfriend, Kyle T.                                Wilkins, Matthew P.dCovariance as an Estimator of Orbit Prediction Error Growth in the Presence of Unknown Sensor Biases=Alfriend, Kyle T.                                Lim, Jong-IlEPerformance of a Dynamic Algorithm for Processing Uncorrelated TracksPImproved Performance of Repetitive Controllers using Smoothing of Control Inputs:Longman, Richard W.                         Chen, Hong-JenhLongman, Richard W.                         Giese, Guido                                  Bock, H. GeorgHThe Optimized Interaction Forces in Minimum Time Control of Elbow Robots6Longman, Richard W.                     Plotnik, Aaron^Subtleties in the Use of Zero-Phase Low-Pass Filtering and Cliff Filtering in Learning ControltWie, Bong                                          Lu, Jianbo                                          Bailey, DavidDNonlinear Feedback Control Logic for Jerk-Free, Rapid Slew Maneuvers�(Wie, Lu) Arizona State Univ, Tempe, AZ 85287-6106, Voice: 602-965-8674, Fax: 602-965-1384, [email protected] (Bailey) Satellite Systems Operation, Honeywell Inc., Glendale, AZ 85308-9650?Fonseca, Ijar M.                              Bainum, Peter M. �Integrated Structural and Control Optimization of a Large Space Structure Subject to the Gravity-Gradient Torque by Using Analytical Sensitivity Analysis�(Fonseca) National Institute for Space Research - INPE, 12223-970 S.J. Campos, S.P., Brazil, Voice: 55-12-329-7242, [email protected] (Bainum) Howard Univ, 2300 6th Street, NW, Washington DC, 20059, Voice: 202-806-6612, [email protected]Preliminary Planning for NEAR's Low-Altitude Operations at 433 ErosBBanerjee, Arun K.                             Singhose, William E.>Kawaguchi, Jun                                Yoshikawa, ShojiAMomentum Dumping with Vibration Reduction for Flexible Spacecraft�(Misra, Sedlak, Gregory, Jones, Smilek) Computer Sciences Corp, 4300 Forbes Blvd, Lanham, MD 20706, Voice: 301-552-0506, Fax: 301-552-3028, [email protected] (Lorentz) SGT, Inc., Greenbelt, MD (Bowser, Mylod) Space Imaging, Denver, COOLandsat-4 Attitude Recovery and Other Experiences with Aging Landsat Spacecraft?Martinot, V.                                       Vignaux, D. VEarth-Centered Angle Station-Keeping in Low-Earth Orbits with Yaw-Steering ConstraintsGirdwood_abs1.docCDesign and Analysis of Space Station Based Micro-Satellite NetworksmYuan, Jianping                                  Fang, Qun                                           Wei, Juan�College of Astronautics, Northwestern Polytechnical Univ, Xi'an, 710072, P.R. China, Voice:  (86)29-8493685, Fax: (86) 29-8491000, [email protected]Dou, Xiaomu                                     Huang, Ying                                       Luo, Jianjun8Orbit Analysis of the Adjoint Satellite to Space Station�College of Astronautics, Northwestern Polytechnical Univ, 710072, Xi'an, P.R. China, Voice:  (86)29-8493685, Fax: (86)29-8491000, [email protected]Ying, Shuh-Jing (Benjamin)5Rotational Motions of a Satellite in a Circular Orbit�Dept of Mechanical Engineering, Univ of South Florida, 4202 East Fowler Avenue, ENB 118, Tampa, FL 33620-5350, Voice: 813-974-5627, Fax: 813-974-3539, [email protected]:Kantsiper, Brian Dr.                         Drake, Howard2Using Tessellations for Large Constellation Design�Wilson, M.G.                                      Johannesen, J.R.                             Halsell, C.A.                                      Haw, R.J.                                             Pojman, J.L.1Post Galileo-Europa-Mission Satellite Tour DesignPNear Earth Asteroid Rendezvous (Near) Revised EROS orbit Phase Trajectory Design9Pickard, Henry                                 Hope, AlanGAdaptation of a Spaceborne Geolocation System to an Airborne ExperimentRelative Motion, Stationkeeping???DSims, Jon A.                                      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Smith, John C.                           Braun, Robert D., Dr.8Colasurdo, Guido                       Casalino, Lorenzo�Dipartimento di Energetica - Politecnico di Torino C.so Duca degli Abruzzi 24, 10129 Torino, Italy, Voice: +39-011-564-4426, Fax: +39-011-564-4599, [email protected]Trajectories towards Near-Earth-Objects Using Solar Electric PropulsionUOptimal DeltaV-Earth-Gravity-Assist Trajectories in the Restricted Three-Body ProblemrJesus, Antonio Delson Conceicao de; Souza, Marcelo Lopes Loiveira e; Prado, Antonio Fernando Bertachini de AlmeidaMMonte-Carlo Analysis of Nonimpulsive Orbital Transfers Under Thrust Errors, 1AAS1.docbRobertson, Michael                      Singhose, William                           Banerjee, ArunAInitial Guess Schemes for Generating Deflection-Limiting CommandsUeno, SeiyaZTranslational Motion of Gravity Gradient Stabilized Satellites Due to Attitude Oscillation�Yokohama National Univ, 79-5 Tokiwadai Hodogaya-ku, Yokohama, 240-8501 Japan, Voice/Fax: +81-45-339-4242, [email protected]McLaughlin, Craig A.                     Gold, Kenn                                         Born, George H.2Altitude Effects on Autonomous Orbit Determination�(McLaughlin) Air Force Research Lab/VSSS, 3550 Aberdeen Ave., SE, Kirtland AFB, NM 87117-5718, Voice: 505-853-6545, Fax: 505-846-6053, [email protected] (Gold, Born) Univ of Colorado, Campus Box 428, Boulder, CO 80309-0428, Voice: 303-492-8638Date
Cumulative
Count by daysMazzoleni, Andre P.iSchaub, Hanspeter                         Vadali, Srinivas R.                           Alfriend, Kyle T.=Spacecraft Formation Flying Control Using Mean Orbit Elements~Lisa Willingham, Texas A&M Univ, College Station, TX 77843-3141, Voice: 409-845-3947, Fax: 409-845-6051, [email protected]McRonald, Angus D.AA Light-Weight Inflatable Hypersonic..Drag Device for Venus Entry/Jet Propulsion Lab, [email protected]Launch VehicleMission Design
NavigationTrajectory OptimizationAttitude EstimationOptimizationAsteroids??StationkeepingOrbit DeterminationAttitude Control
ConstellationTether, Attitude ControlTether Optimization, RendezvousAstrodynamics Solar SailClose Approach, Relative MotionPrediction Uncertainty(Trajectory Optimization, Relative MotionAerogravity, OptimizationAttitude TheoryArchitectureFormation Flying	AsteroidsLambertAsteroids, AstrodynamicsAttitude-Flexible BodyReentry, Mission Design	StandardsPrediction ErrorAttitude, AstrodynamicsDrag Modelling?AsteroidTether, Orbit DeterminationOptimization, AstrodynamicsAtmospheric ModelingAtmopsheric ModelingClose Approach ConstellationsBreakupsTetherOrbit Determination Accuracy�Tolson, R.H.                                     Keating, G.M.                                    Baird, D.T.                                          Noll, S.N.                                             Shellenberg, T.I.OUtilization of Mars Global Surveyor Accelerometer Data for Atmospheric ModelingMackison, Donald L.�Jet Propulsion Lab, California Institute of Technology, MS 301-125J, 4800 Oak Grove Drive, Pasadena, CA 91109-8099, [email protected]�The Charles Stark Draper Lab, 2200 Space Park Dr, #210, Houston, TX 77058, Voice: 281-333-2198, Fax: 281-333-5276, [email protected]�NASA Programs, The Aerospace Corp, 2101 NASA Rd One, Bldg 45, Rm 650, Houston, TX 77058, Voice: 281-483-3263, Fax: 281-483-9677, [email protected]�The Charles Stark Draper Lab, 2200 Space Park Dr, #210, Houston, TX 77058, Voice: 281-333-2127, Fax: 281-333-5276, [email protected]�GRC International, Inc, 985 Space Center Dr, #310, Colorado Springs, CO 80915, Voice: 719-596-5395, Fax: 719-596-6139, [email protected]�INTELSAT, Box#60, 3400 International Dr NW, Washington DC 20008-3098, Voice: 202-944-7581, Fax: 202-944-7032, [email protected]North Carolina A&T State Univ, 1601 East Market St, Greensboro, NC 27411, Voice: 336-334-7620, Fax:336-334-7417, [email protected]The Charles Draper Lab, 555 Technology Square, Cambridge, MA 02139, Voice: 617-258-2433, [email protected]�Naval Research Lab, Code 8233, 4555 Overlook Ave SW, Washington DC 20375-5355, Voice: 202-404-8337, Fax: 202-404-7785, [email protected]The MITRE Corp, 1150 Academy Park Loop, #212, Colorado Springs, CO 80910-3716, Voice: 719-572-8383, [email protected]Sess 5Mon PM?Fisher, Jeff Wesley                        Trochman, William R.ATheory and Flight Performance of the Magnetic Orbital GyrocompassAbstractSubmittalAbstract1_AK.docD'Souza, Christopher N.IOptimal Two-Impulse and Three-Impulse Maneuvers for Mars orbit RendezvouseGates, Stephen S.                          Koss, Stephen M.                          Zedd, Michael F.CLessons Learned About the Deployment Malfunction of the ATEx TetherMiller, James G.+Velocity Distribution of Satellite BreakupsLang, Thomas J.RCharacteristics of Crosslinks Between Satellites in Large Symmetric ConstellationsmStevens, H.D.                                    Rodden, J.J.                                      Carrou, S.8Mass Expulsion Control for Precision Pointing Spacecraft�(Gabor) AFRL and Univ of Texas Center for Space, [email protected] (Nerem) Univ of Texas Center for Space Research, [email protected]          Lyons, Daniel T. Dr.gAerobraking at Venus and Mars: A Comparison of the Magellan and Mars Global Surveyor Aerobraking Phases7Woodburn, James                          Ohlarik, DeronaA Graphical Method for the Computation of Antenna Obscuration for the International Space Station�Calibration of Radiometric Data for General Relativity and Solar Plasma during the Near Earth Asteroid Rendezvous Spacecraft Solar Conjunction?Weeks, C.J.                                        Miller, J.K.AGist, Robert G.                                  Oltrogge, DanieleCollision Vision: Covariance Modeling and Intersection Detection for Spacecraft Situational AwarenessYParametric Analysis for the Selection of Data Source in the Orbit Determination ProcessesiBir, Megan Lt.                                   Carter, Scott Capt.                         Sabol, ChrisCangahuala, L.A.�Carter, Scott Capt.                         McLaughlin, Craig Dr.                    Sabol, Chris Dr.                                Bir, Megan Lt.�National Institute for Space Research - INPE, Space Mechanics and Control Division - DMC, CEP 12201-970, Sao Jose dos Campos, Brazil, [email protected]�Jet Propulsion Lab, California Institute of Technology, 4800 Oak Grove Dr, Pasadena, CA 91109-8099, Voice: 818-354-8101, Fax: 818-393-6558, [email protected]�Jet Propulsion Lab, California Institute of Technology, MS 301/125J, 4800 Oak Grove Dr, Pasadena, CA 91109-8099, Voice: 818-354-4321yGeorgia Institute of Technology, Atlanta, GA 30332-0150, Voice: 404-894-9526, Fax: 404-894-2760, [email protected]�Univ of Illinois at Urbana-Champaign, MC-236, 306 Talbot Lab, 104 S. Wright St, Urbana, IL 61801, Voice: 217-333-0678, Fax: 217-244-0720, [email protected] (Prussing) Voice: 217-333-8231�Univ of Illinois at Urbana-Champaign, MC-236, 306 Talbot Lab, 104 S. Wright St, Urbana, IL 61801, Voice: 217-333-0678, Fax: 217-244-0720, [email protected]The Charles Stark Draper Lab, 555 Technology Square, Cambridge, MA 02139-1000, Voice: 617--258-2433, [email protected]�(Mase, Spencer, Smith) Jet Propulsion Lab, California Institute of Technology, 4800 Oak Grove Dr, Pasadena, CA 91109-8099, Voice: 818-354-8990, Fax: 818-393-5261, [email protected] (Braun) NASA Langley Research Center�Aerospace<   Engineering Dept, 211 Aerospace Engineering Bldg, Auburn Univ, Auburn, AL 36849-5338, Voice: 334-844-6820, Fax: 334-844-6803, [email protected]Sess 16Wed PM�Orbit Dynamics Section, Space Systems/LORAL, MS G-76, 3825 Fabian Way, Palo Alto, CA  94303, Voice: 650-852-407, Fax: 650-852-4666, [email protected]SAIC, 1501 Woodfield Road, #202 N, Schaumburg, IL  60173, Voice: 847-330-2518, Fax: 847-330-2522, [email protected]Space Systems/LORAL, MS G-76, 3825 Fabian Way, Palo Alto, CA  94303, Voice: 650-852-4909, Fax: 650-852-4666, [email protected]Space Dept, Johns Hopkins Univ, APL, Laurel, MD 20723-6099, Voice: 240-228-5206, Fax: 240-228-1093, [email protected]�Lockheed Martin Missiles & Space, Advanced Technology Center, 3251 Hanover Street, Bldg 250, Org H1-61, Palo Alto, CA  94304, [email protected]{The Aerospace Corp, MS M4/947, POB 92957, LAX, CA 90009, Voice: 310-336-1422, Fax: 310-336-5827, [email protected]�The Charles Stark Draper Lab Fellow, AFIT/CIGG-DET 365, MIT, 555 Technology Square, MS 70, Cambridge, MA  02139, Voice: 617-258-2094, Fax: 617-258-2772, [email protected]POB 250, College of Astronautics, Northwestern Polytechnical Univ, Xi'an   710072, the People's Republic of China�Space Systems/LORAL, MS Z01, 3825 Fabian Way, Palo Alto, CA  94303-4604, Voice: 650-852-6197, Fax: 650-852-4661, [email protected]�Naval Research Lab, 4555 Overlook Ave SW, Washington DC 20375-5355, Voice: 202-767-0432, Fax: 202-404-7516, [email protected]�Facility of Aerospace Engineering, Israel Institute of Technology, Technion City, Haifa, 32000, Israel, Voice: 972-4-829-3020, Fax: 972-4-823-0956, [email protected]Ellipso, Inc, 1133 21st St, NW, 8th Floor, Washington, DC, 20036, Voice: 202-466-4488, Fax: 202-466-4493iEastern Connecticut State Univ, Math/CSC Dept, 83 Windham St, Willimantic, CT  06226, Voice: 860-465-5000�Hughes Space & Communications, 2000 E. El Segundo Blvd, POB 902, El Segundo, CA 90245-4709, Voice: 310-416-5127, Fax: 310-416-5188, [email protected]Glover, Robert A.                         Schumacher, Paul W. Jr.DThe Y2K Effort for the Naval Space Command Mission Processing System�(Glover) GRCI, 985 Space Center Drive, #310, Colorado Springs, CO  80915, Voice: 719-596-5395, Fax: 719-596-6139, [email protected] (Schumacher) Naval Space Command, Dahlgren, VA�(Gefert) NASA , John Glenn Research Center at Lewis Field, 21000 Brookpark Rd, MS 500-201, Cleveland, OH, Voice: 216-977-7117, Fax: 216-977-7125, [email protected] (Hack) Voice: 216-977-7060, [email protected]�Jet Propulsion Lab, California Institute of Technology, M/S 301-276, 4800 Oak Grove Dr, Pasadena, CA 91109-8099, Voice: 818-354-2567, Fax: 818-393-5214, [email protected]�Dept of Eng, Texas Christian Univ, Box 298640, Fort Worth, TX 76129, Voice: 817-257-6317, Fax: 817-257-7704, [email protected]�(F.O.) Univ of California, One Shields Ave, Davis, CA 95616-5294, Voice: 530-752-2309, Fax: 530-752-4158, [email protected] (E.M.) 6000 J St, Sacramento, CA 95819-60312Stationkeeping and Proximity Operations - Todd ElyTues PMSess 12Wed AMSess 3Sess 15Combine with #79Mon AMSess 1�Cefola, Paul                                           Nazarenko, A.                                       Proulx, R.                              Yurasov, V.Atmospheric Density (Marcos)HViereck, Rodney                                          Joselyn, Jo AnnDThe Solar Cycle and its Effect on Neutral Density and Satellite DragRNOAA Space Environment Lab, 325 Broadway, Boulder, CO 80303, [email protected]Pardini, C.                               Anselmo, L..[email protected]; [email protected]�Tolson, R.H.                               Keating, G.M.                          Baird, D.T.                           Noll, S.N.                             Shellenberg, T.I.[email protected]?Methods of Orbit Determination for EllipsoTM Sub-Constellations7Orbit Analysis Tools Software (Version 1 for WindowsTM)1Formation Flying Near the Sun-Earth/Moon L1 Point)+	Session #2Asteroids and Comets - Victoria Coverstone-Carroll!Orbit Determination - David CicciThis is a duplicate of # 47This is a duplicate of # 31!Mission Design: Mars - Bob Melton*Formation Flying/Constellations Jerry Beck'Attitude Control: Theory - Peter Bainum+Orbit Determination: Missions - Jay Middour*Solar Sails and Low Thrust - Claig Kluever%Topics in Control Theory - Tom Carter.Launch and Mission Support Tools - Les Scakett�CNUCE, via S. Maria 36, I-56126 Pisa, Italy, Fax: +39-050-904052 (Pardini), Voice: +39-050-593328, [email protected] (Anselmo), Voice: +39-050-593220, [email protected]Markopoulos, Nikos�School of Aerospace Engineering, Georgia Institute of Technology, 270 Ferst Drive, Atlanta, GA  30332-0150, Voice: 404-894-3066, Fax: 404-894-2760, [email protected]An Operational Approach for Generating Near-Optimal Station Keeping Strategies via Parallel Genetic Algorithms�Smith, James E., 2LT, USAF                     Proulx, Ronald J.                    Cefola, Paul J.                        Draim, John E.]How Much Thrust, Energy, or Propellant Does it take to Guide a Natural Celestial Body? (None)IAquarius, a Low-Cost, Low-Reliability Launch Vehicle to Carry Consumables.Rendezvous Mission to a First-Apparition Comet>Image Navigation Based on Landmark and Earth Edge MeasurementsCOptimal Low-Thrust Earth-Moon Targeting Strategy for N-Body ProbleMcPrecision Attitude Estimation with Star Trackers: Experience, Error Models an Their Interpretation 4Numerical Research in Non-Coplanar Orbital ManeuversqCalibration of Semi-Empirical Atmosphere Models through the Orbital Decay of Spherical and Cylindrical Satellitesaasabsprado.docqThe Optimization of Continuous Constant Acceleration Transfer Trajectories in the Presence of the J2 Perturbation51999_Astro_Submittal.doc; 1999_Astrodynamics_Conf.doc:Friedlander, Alan                            Niehoff, JohnoFengqi, Zhou                                    Hui, Liao,                                            Jun, ZhouMApplication of Extended Kalman Filter for Small Satellite Attitude EstimationSrinivasan, B.�Orbit Determination of Geo-Stationary Satellites Using a Parabolic Sinusoidal Fit for Longitude and a Sinusoidal Fit for the Sine of Declination~INSAT-Master Control Facility, Dept of Space, Government of India, Hassan-573201, Karnataka State, India, Fax: 0091-8172-67423rExponential Stabilization of Spacecraft's Angular Velocity with Underactuated Configuration of One-Sided ThrustersmZhang, Bing                                       Wu, Hongxin                                     Zhang, HongbKamel, Ahmed, Dr.                      Gelon, Walter                               Reckdahl, KeithGA Practical Stationkeeping Method for Modular Geosynchronous Satellites\Elliptical Sun-Synchronous Orbits with Line of Apsides Lying In or Near the Equatorial Plane�Draim, John E.                                   Cefola, Paul J.                                 Proulx, Ronald J.                           Larsen, Duane                             Granholm, George<Biswell, Brian L.                          Puig-Suari, JordiAerobrakingLaunch Vehicle, OptimizationMission Design, Tools
AstrodynamicsControl, RobotsControl Accuracy, CovarianceClose ApproachMission Control	FormationLaunch Vehicle, Mission Design
Solar SailxBell, Julia L.                               Lo, Martin W.                                               Wilson, Roby S.Genesis Trajectory DesignvJet Propulsion Lab, California Institute of Technology, 4800 Oak Grove Dr, Pasadena, CA 91109, [email protected]Beckman, Mark                       Guzman, Jose J.Triana Mission Design>Venus Surface Sample Return: A Weighty High-Pressure ChallengeVSSR.pdfxJet Propulsion Lab, California Institute of Technology, 4800 Oak Grove Dr, Pasadena, CA 91109, [email protected]�Sweetser, Ted                  <          Cameron, Jonathon              Chen, Gun-Shing                     Cuts, Jim; Gershman, Bob, Gilmore, Martha S.               +10 other authors                                                EAltitude Control of a Tethered Lifting Probe for Atmospheric Research;Improved Tether Aerobraking Maneuvers Using a Lifting Probe�(Biswell) Raytheon Systems Company, MS 805/M4, POB 11337, Tucson, AZ  85734-1337, [email protected], Voice: 520-794-8719 (Puig-Suari) Aeronautical Engineering Dept, California Polytechnic Univ, San Luis Obispo, CA  93407Tsiotras, PanagiotisWFeasible Trajectory Generation for Underactuated Spacecraft Using Differential Flatness�School of Aerospace Engineering, Georgia Institute of Technology, 270 Ferst Drive, Atlanta, GA  30332-0150, Voice: 404-894-9526, Fax: 404-894-2760, [email protected]Carter, Thomas E.cNecessary and Sufficient Conditions for Optimal Impulsive Rendezvous and Linear Equations of Motionvan de Kolk, Christel>Stability of Levitated Cylindrical Orbits by Using Solar Sails�Univ of Tennessee Space Institute, MS 26, 411 B.H. Goetheet Parkway, Tullahoma, TN  37388-9700, Voice: 931-393-7103, [email protected]�Williams, Kenneth E.                   Hong, Philip E.                             Zietz, Richard P.                          Han, Don:Maneuver Design and Calibration for the Genesis SpacecraftPeck, Mason VMass-Properties Estimation for Spacecraft with powerful Fuel Damping Extended AbstractAdamo, Daniel R.RContingency ISS Rendezvous Recovery Planning by Houston and Moscow Control Centers8Markley, F. Landis                      Mortari, Daniele1How to Estimate Attitude from Vector Observations�(Markley) NASA's Goddard Space Flight Center, Greenbelt, MD, [email protected] (Mortari) Univ of Rome "La Sapienza", Rome, Italy;Rauwolf, Gerald                           Friedlander, AlanENear-Optimal Solar Sail Trajectories Generated by a Genetic AlgorithmWright, James R. ,Close Approach Spacecraft Maneuver Criterion:Chesley, Steve                              Milani, Andrea<Nonlinear Methods for the Propagation of Orbital Uncertainty5Asteroid Close Encounters with Earth: Risk Assessment�Dipartimento di Matematica, Via Buonarroti 2, 56127 Pisa, Italy, Voice: +39-050-844274, Fax: +39-050-844224, [email protected]MacMission Control, 4203 Moonlight Shadow Court, Houston, TX 77059-5525, Voice: 281-480-9631, [email protected]Nicholas, A.C.                              Picone, J.M.                                 Thonnard, S.E.rA Methodology for using optimal MSIS Parameters Retrieved from SSULI Data to Compute Satellite Drag on LEO Objects 2/19/99Ely, Todd A., Dr.NImpact of Eccentricity on East-West Stationkeeping for the GPS Class of OrbitsePetropoulos, Anastassios E.         Longuski, James M.                         Vinh, Nguyen X.       SAnalytic Representations of Low-Thrust Trajectories for Gravity-Assist Applications�Purdue Univ, 1282 Grissom Hall, West Lafayette, IN 47907-1282, Voice: 765-494-5139, Fax: 765-494-0307, Home Voice: 765-423-1287, [email protected] (Vinh) Univ of MichiganBJavorsek, Daniel II                        Longuski, James M.     FVelocity Pointing Errors Associated with Spinning Thrusting Spacecraft[Periodic Solutions for a Spinning Asymmetric Rigid Body with Constant Principal-Axis TorqueBonfiglio, Eugene P.                        Longuski, James M.                                Vinh, N.X.                       3Automated Design of Aerogravity-Assist Trajectories�Purdue Univ, 1282 Grissom Hall, West Lafayette, IN 47907-1282, Voice: 765-494-5139, Fax: 765-494-0307, Home Voice: 765-423-1287, [email protected]Carranza, Eric                               Konopliv, Alex                             Ryne, MarkaLunar Prospector Orbit Determination Uncertainties Using the High Resolution Lunar Gravity Models�Hall, Robert A.                             Kirchwey, Kim                             Martin, Michael                           Rosch, Gene                                 Zimpfer, DouglasJFlight Control Overview of STS-88, the First Space Station Assembly FlightSmith, Robert H.[An Axiomatic Design Approach Applied to the Problem of Comparing Space System ArchitecturesAThe Naval Space Command Automatic Differential Correction Process�Danielson, Don A.                          Canright, D.                              Perini, Deborah, N.                     Schumacher, Paul W.�(Danielson/Canright) Dept of Mathematics, Code MA/Dd, Rm Glasgow 341, Naval Postgraduate School, Monterey, CA 93943-5216, Voice: 831-656-2622, Fax: 831-656-2355, [email protected] (Perini/Schumacher) Naval Space Command, Dahlgren, VA 22448 Bedrossian, Nazareth8Space Station Attitude Control During Payload OperationsKOn the Improved orbit Stability Criterion Around An Irregularly Shaped Body#Navigation of Mars Mission - NOZOMI.Ichikawa, Tsutomu                 Kato, Takaji�The Institute of Space and Astronautical Science, 3-1-1 Yoshinodai, Sagamihara, Kanagawa 229-8510, Japan, Voice/Fax: 81-42-759-8357, [email protected]�Folta, David                                 Gramling, Cheryl                          Leung, Dominic                               Belur, Sheela                                 Long, Anne-Autonomous Navigation Using Celestial Objects�(Folta/Gramling) NASA Goddard Space Flight Center, Code 571, Greenbelt, MD 20771, Voice: 301-286-6082, Fax: 301-286-1719, [email protected] (Leung/Belur/Long) Computer Sciences Corporation�Folta, David                                 Beckman, Mark                          Lozier, David                            Galal, Ken�The Lunar Prospector Mission: Final Results of Trajectory Design, Quasi-Frozen Orbits, Extended Mission Targeting, and the Lunar Topography and Potential Models�(Folta/Beckman) NASA Goddard Space Flight Center, Code 571, Greenbelt, MD 20771, Voice: 301-286-6082, Fax: 301-286-1719, [email protected] (Lozier/Galal) Ames Research Center, NASASonnabend, DaveToubles with LambertuAnalytical Engineering, 5423 Glendale Gulch, Boulder, CO 80301-3537, Voice: 303-530-9641, [email protected](Europa Orbiter Mission Trajectory DesignAbst AAS 99 Europa Orbiter.doc9Johannesen, Jennie R.                  D'Amario, Louis A.5Low Earth Orbit Estimation from Single Ground StationCCurti, F.                                               Parisse, M.�Centro di Ricerca Progetto San Marco, Univ of Rome "La Sapienza", Via Salaria 851, 00138 Rome, Italy, Voice: +39-06-8120530, Fax: +39-06-8105241, [email protected]	CURTI.docRIC Abs.docUlivieri.doc�Cesarone, R.J.                                 Hastrup, R.C.                                    Bell, D.J.                                             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Astrodynamics�---�DZ;lM@�?�/�Fh��E�f/F����p����*���<l���@��@b��b��b���b��bb��b@b����������������@����b��0������bb��b�������l������@��@����b��T0�����_@<���@<���@�Menon, Premkumar R.0�'Stardust Navigation Covariance Analysis���Jet Propulsion Lab, 4800 Oak Grove Dr, California Institute of Technology, Pasadena,  CA 91109, Voice: 818-354-5093, [email protected]�AIAA99 Abstract.doc�$Accuracy, Covariance��---��`@<���@<���@Y�PHerman, Albert L., PhD                                         Spencer, David B.=�4Optimal, Low-Thrust, LEO to GEO/MEO/HEO Trajectories���(Herman) Spectrum Astro, Inc, 1440 North Fiesta Blvd., Gilbert, AZ 85233, Voice: 602-892-8200, Fax: 602-892-2949, [email protected] (Spencer) Air Force Research Laboratory/VSSS, Kirtland AFB, NM 87117-5776, [email protected] -�$Abstract~from~Herman~and~Spencer.doc�$Optimization��---�� `@<���@<���@���D'Amario, Louis A.                     Bollman, Willard E.                          Lee, Wayne J.                                    Roncoli, Ralph B.                             Smith, John C. S�JMars Orbit Rendevous Strategy for the Mars 2003/2005 Sample Return Mission��Jet Propulsion Lab, California Institute of Technology, 4800 Oak Grove Dr, MS 301-276, Pasadena, CA 91109, Voice: 818-354-3209, Fax: 818-393-5214, [email protected], [email protected], [email protected], [email protected]$�MSR Rendezvous Abstract.doc�$Mission Design��---��@`@<���@<���@�Cangahuala, L.A.P�GThe Gravitational Potential of a Body in Terms of Ellipsoidal Harmonics���Jet Propulsion Lab, 4800 Oak Grove Dr, California Institute of Technology, MS 301-125J,  Pasadena, CA, Voice: 818-354-3606, [email protected])� Ellipsoidal.abstract.2.10.99.doc�$
Astrodynamics��---��``@<���@<���@�Powell, Thomas D.\�SAutomated Tuning of an Extended Kalman Filter using the Downhill Sismplex Algorithm��{The Aerospace Corp, POB 92957, M4/962, LAX, CA 90009-2957, Voice: 310-336-5572, Fax: 310-336-1812, [email protected]��$Orbit Determination��---���`@<���@<��@�Lyons, Daniel T. Dr.p�gAerobraking at Venus and Mars: A Comparison of the Magellan and Mars Global Surveyor Aerobraking Phases���Jet Propulsion Lab, California Institute of Technology, Pasadena,  CA 91109, Voice: 818-393-1004, Fax: 818-393-3147 [email protected]��$Aerobraking��---���`@<���@<��@@�7Woodburn, James                          Ohlarik, Deronj�aA Graphical Method for the Computation of Antenna Obscuration for the International Space Station��xAnalytical Grahpics, Inc, 325 Technology Dr, Malvern, PA 19335, Voice: 610-578-1000, Fax: 610-578-1001, [email protected]��$
Astrodynamics��---���`@<���@<��@H�?Weeks, C.J.                                        Miller, J.K.���Calibration of Radiometric Data for General Relativity and Solar Plasma during the Near Earth Asteroid Rendezvous Spacecraft Solar Conjunction��(Weeks) Loyola Marymount Univ, 7900 Loyola Blvd, LAX, CA 90045-8130, Voice: 310-338-5108, Fax: 310-338-7339, [email protected] (Miller) Jet Propulsion Lab, California Institute of Technology, MS 301/125j, 4800 Oak Grove Dr, Pasadena,  CA 91109, Voice��$
Navigation��---���`@<���@<��@J�AGist, Robert G.                                  Oltrogge, Danieln�eCollision Vision: Covariance Modeling and Intersection Detection for Spacecraft Situational Awareness���The Aerospace Corp, POB 92957, M4/946, LAX, CA 90009-2957, Voice: 310-336-4297, Fax: 310-336-5827, [email protected] (Oltrogge) Voice: 719-554-6026, Fax: 719-554-5876, [email protected]��$Close Approach��---��a@<���@<��@r�iBir, Megan Lt.                                   Carter, Scott Capt.                         Sabol, Chrisb�YParametric Analysis for the Selection of Data Source in the Orbit Determination Processes��(Bir) Air Force Research Lab/VSSS, 3550 Aberdeen Ave SE, Kirtland AFB, NM 87117-5718, Voice: 505-853-4136, Fax: 505-846-6053, [email protected] (Carter) Voice: 505-853-3970, Fax: 505-846-0033, [email protected] (Sabol) Voice: 505-846-4056, Fax: 50��$Orbit Determination��---�� a@<���@<��@���Carter, Scott Capt.                         McLaughlin, Craig Dr.                    Sabol, Chris Dr.                                Bir, Megan Lt.]�TSpaceflight Dynamics Support for the MightySat II.1 Hyperspectral Payload Operations��(Carter) Air Force Research Lab/VSSS, 3550 Aberdeen Ave SE, Kirtland AFB, NM 87117-5718, Voice: 505-853-3970, Fax: 505-846-0033, [email protected] (McLaughlin) Voice: 505-853-6545, Fax: 505-846-6053, [email protected] (Sabol) Voice: 505-846-4056, Fax: ��$Mission Control��---��@a@<���@<��@���Carter, Scott Capt.                         Sabol, Chris Dr.                                Burns, Richard                                 Bir, Megan Lt.8�/A Fresh Look at Angles-Only Orbit Determination��(Carter) Air Force Research Lab/VSSS, 3550 Aberdeen Ave, SE, Kirtland AFB, NM 87117-5718, Voice: 505-853-3970, Fax: 505-846-0033, [email protected] (Sabol) Voice: 505-846-4056, Fax: 505-846-6053, [email protected] (Burns) Voice: 505-846-2352, Fax: 505-84��$
Astrodynamics��---��`a@<���@
�< �Desai, Prasun N. Q�HEntry Dispersion Analysis for the Muses-C Asteroid Sample Return CapsuleF�=NASA Langley Research Center, MS 365, Hampton, VA 23681-2199 ��$Mission Design��---���a@<���@<��@�Park, Sang-Youngq�hThermally-Induced Attitude Vibration Control of a Spacecraft with a Flexible Boom Using Smart Structures�vNaval Postgraduate School, 699 Dyer Rd, Bldg 245, Monterey, CA 93943-5000, Voice: 408-656-2656, [email protected]��$Attitude Control��---���a@<���@<��@���Esposito, P.B.; Alwar, V.                                               Burkhart, P.D.; Demcak, S.W.                                   Graat, E.J.; Johnston, M.                                                       Portock, B.M. V�MNavigating Mars Global Surveyor through the Martian Atmosphere: Aerobraking 2���Jet Propulsion Lab, California Institute of Technology, 4800 Oak Grove Dr, Pasadena, CA 91109, Voice: 818-393-1264, Fax: 818-393-3147, [email protected]��$Aerobraking��---���a@<���@<���@B�9Johannesen, Jennie R.                  D'Amario, Louis A.1�(Europa Orbiter Mission Trajectory Design��zJet Propulsion Lab, California Institute of Technology, 4800 Oak Grove Dr, Pasadena, CA 91109, [email protected]'�Abst AAS 99 Europa Orbiter.doc�$Mission Design��---���a@<���@<���@L�CCurti, F.                                               Parisse, M.>�5Low Earth Orbit Estimation from Single Ground Station���Centro di Ricerca Progetto San Marco, Univ of Rome "La Sapienza", Via Salaria 851, 00138 Rome, Italy, Voice: +39-06-8120530, Fax: +39-06-8105241, [email protected]�	CURTI.doc�$Orbit Determination��---��b@<���@<���@���Cesarone, R.J.                                 Hastrup, R.C.                                    Bell, D.J.                                             Roncoli, R.G.[�RArchitectural Design for a Mars Communications & Navigation Orbital Infrastructure~�uJet Propulsion Lab, California Institute of Technology, 4800 Oak Grove Dr, Pasadena, CA 91109, [email protected]�RIC Abs.doc�$Mission Design��---�� b@<���@<���@�Ulivieri, Carlo`�WThe Multi-Synchronous Technique for Environment Monitoring by a Satellite Constellation���Centro di Ricerca Progetto San Marco, Univ of Rome "La Sapienza", Via Salaria 851, 00138 Rome, Italy, Voice: +39-06-8120539, Fax: +39-06-8106351, [email protected]�Ulivieri.doc�$
Constellation��---��@b@<���@<���@r�iBarnds, Jim                                       Coffey, Shannon                             Davis, Mark0�'Tracking of the TiPS Tethered Satellite#�[email protected]��$Tether��---��`b@<���@<���@t�kHarvie, Edwin                                    Phenneger, Milt                               Dress, AndreZ�QMagnetic Precession Attitude Dynamics for On-Orbit Storage of the GOES Spacecraft��(Harvie) ASRC Aerospace, 6411 Ivy Ln, #610, Greenbelt, MD 20770, Voice: 301-345-4500 X229, Fax: 301-345-9274, [email protected] (Phenneger) X231, [email protected] (Dress) NOAA, Dept of Commerce, FOB#4, Suitland, MD 20746, Voice: 301-457-5��$Attitude Control��---���b@<���@<���@��Lemoine, F.G.                                   Rowlands, D.D.                                 Smith, D.E.; Pavlia, D.E.                                 Chinn, D.S.; Luthcke, S.B.                                            Neumann, G.A.                   D�;Orbit Determination for Mars Global Surveyor during Mapping��(Lemoine, Rowlands, Smith) Lab for Terrestrial Physics, NASA Goddard Space Flight Center, Code 926, Greenbelt, MD 20771, Voice: 301-614-6109, Fax: 310-614-6099, [email protected] (Pavlia, Chinn, Luthcke) Raytheon ITSS, Greenbelt, MD (Neumann, Zu��$Orbit Determination��---���b@<���@<���@~�uMiller, Andrew J.                              Gray, Gary L.                                      Mazzoleni, Andre P.q�hNonlinear Dynamics of a Viscously Damped Spacecraft with a Flexible Appendage and Time-Dependent Forcing���The Pennsylvania State Univ, 227 Hammond Bldg, Univ Park, PA 16802-1401, Voice: 814-865-4523, Fax: 814-863-7967, [email protected]��$Attitude Control��---���b@<���@<���@r�iToniolo, Matthew D.                      Lee, Mokin                                         Gray, Gary L.���Comparison of Melnikov's Method and Numerical Simulation for Predicting Nonlinear Dynamics in the Pitch Motion of Actively Controlled Satellites in a Gravity Gradient Field���The Pennsylvania State Univ, 227 Hammond Bldg, Univ Park, PA 16802-1401, Voice: 814-865-4523, Fax: 814-863-7967, [email protected]��$Attitude Theory��---~
�9�b@��<<+�8"This was a duplicate - leave blank��$---��c@<���@<��@l�cDress, Andre                               Harvie, Edwin                            Phenneger, Milt[�RControl Methods for the Activation and Operation of the GOES On-Orbit Storage Mode��(Dress) NOAA, Dept of Commerce, FOB#4, Suitland, MD 20746, Voice: 301-457-5180 X196, Fax: 301-457-5175, [email protected] (Harvie) ASRC Aerospace, 6411 Ivy Ln, #610, Greenbelt, MD 20770, Voice: 301-345-4500 X229, Fax: 301-345-9274, edwin.harvie@akspaN�EStorage Control Abstract(1).doc;      Storage Control Abstract(1).txt�$Attitude Control��---�� c@<��@<��@E�<Hall, Christopher D.                        Beck, Jeffrey A.2�)Relative Equilibria of Orbiting Gyrostats���(Hall) Virginia Polytechnic Institute & State Univ, Blacksburg, VA 24061, Voice: 540-231-2314, Fax: 540-231-9632, [email protected] (Beck) Air Force Research Lab, Kirtland AFB, NM 87117��$Attitude Theory��---��@c@<��@<��@=�4Howell, K.C.                            Barden, B.T.�H�1Formation Flying Near the Sun-Earth/Moon L1 Point)*
+���Purdue Univ, 1282 Grissom Hall, West Lafayette, IN 47907-1282 (Howell) Voice: 765-494-5786, Fax: 765-494-0307, [email protected] (Barden) Voice: 765-494-5813, Fax: Same, [email protected]��$	Formation��---��`c@<��@<��@���Kubitschek, Daniel G.              Gold, Kenneth                         Ondrey, Michael                      Axelrad, Penina                        Born, George H.P�GICESat Attitude Algorithm for Maintained Reference Groundtrack Pointing���Univ of Colorado, Campus Box 431, Boulder, CO 80309-0431, Voice: 303-492-6677, Fax: 303-492-2825, [email protected]��$Attitude Control��---���c@<��@<��@�Chern, Jeng-ShingD�;System Design Considerations for a Formosa-X Microsatellite}�tChung Shan Institute of Science and Technology, POB 90008-6-7, Lungtan, Taiwan 32526, R.O.C., [email protected]�	AAS02.doc�$Mission Design��---���c@<��@<��@�Penzo, Paul A.A�8Venus and Beyond Using the Ariane ASAP Launch Capability���Jet Propulsion Lab, California Institute of Technology, MS 301-140H, 4800 Oak Grove Dr, Pasadena, CA 91109, Voice: 626-354-6162, Fax: 626-393-9900, [email protected]�'�$Launch Vehicle, Mission Design��---���c@<��@<��@�Sauer, Carl G., Jr.H�?Solar Sail Trajectories for Solar Polar and Heliopause Missions���Jet Propulsion Lab, California Institute of Technology, MS 301-140H, 4800 Oak Grove Dr, Pasadena, CA 91109, Voice: 818-354-4875, Fax: 818-393-9900, [email protected]��$
Solar Sail��1---�D^;lc��^��B�@a@jPv���7��ex���F}�<l@�����b��b��b���b��bb��bb��������������������b��0������b@b��b@��@�����l��� �����c@<��@<`��@��xBell, Julia L.                               Lo, Martin W.                                               Wilson, Roby S."�Genesis Trajectory Design�vJet Propulsion Lab, California Institute of Technology, 4800 Oak Grove Dr, Pasadena, CA 91109, [email protected]��$Mission Design��,...��d@<��@<`��@<�3Beckman, Mark                       Guzman, Jose J.�Triana Mission Design��(Beckman) Goddard Space Flight Center, Code 572, Greenbelt, MD 20771, Voice: 301-286-8866, Fax: 301-286-0369, [email protected] (Guzman) Purdue Univ, Grissom Hall 1282, West Lafayette, IN 47907-1282, Voice: 765-494-5132, Fax: 765-494-0307, jguzma��$Mission Design��,...�� d@<@��@<`��@���Sweetser, Ted                          Cameron, Jonathon              Chen, Gun-Shing                     Cuts, Jim; Gershman, Bob, Gilmore, Martha S.               +10 other authors                                                G�>Venus Surface Sample Return: A Weighty High-Pressure Challenge��xJet Propulsion Lab, California Institute of Technology, 4800 Oak Grove Dr, Pasadena, CA 91109, [email protected]�VSSR.pdf�$Mission Design��,...��@d@<`��@<`��@l�cde Lafontaine, Jean               Vuilleumier, Pierrik                 Van den Braembussche, Pieter3�*Autonomous Control of the Proba Spacecraft��(Jean) Universite de Sherbrooke, 2500, boul de l'Universite, Sherbrooke, (Quebec), J1K 2R1, Canada, [email protected] (Pierrik) ESA/ESTEC, Keplerlaan 1, 2201 AZ Noordwijk, the Netherlands (Pieter) Verhaert Design and Development nv, Hogenakk!�AAS AIAA Astrod Conf.doc�$
Navigation��,...��`d@<���@<���@7�.Ichikawa, Tsutomu                 Kato, Takaji,�#Navigation of Mars Mission - NOZOMI���The Institute of Space and Astronautical Science, 3-1-1 Yoshinodai, Sagamihara, Kanagawa 229-8510, Japan, Voice/Fax: 81-42-759-8357, [email protected]��$
Navigation��,...���d@<���@
�< Y�PBinning, Patrick W.                  Middour, Jay                    Soyka, MarkZ�QOrbit Determination Using Space to Ground Differential GPS in NRL's OCEAN Package��3�Naval Research Lab, 4555 Overlook Ave SW, Washington DC 20375-5355, Voice: 202-767-0432, Fax: 202-404-7516, [email protected]��$Orbit Determination��,...���d@<��@<��@�Mackison, Donald L.1�(ATTDES - Generalized Equations of Motion��|Univ of Colorado, Campus Box 429, Boulder, CO 80309-0429, Voice: 303-492-6417, Fax: 303-492-7881, [email protected]�astro99-abstract.doc �$Attitude Control, Tools��,...���d@<@��@<@��@�Matousek, SteveN�ESpaceTime - A MIDEX Proposal to Test Einstein's Equivalence Principle���Jet Propulsion Lab, California Institute of Technology, MS 264-426, 4800 Oak Grove Dr, Pasadena, CA 91109, Voice: 818-354-6689, Fax: 818-393-6800, [email protected]#�Aug 99 AK abs-Matousek.pdf��$,...���d@<���@
�< a�XPourtakdoust, S.H.                        Mehri B.                    Novinzadch, A.R.B.~�uAn Investigation of Satellite Oscillations in an Arbitrary Orbit Using Regular Perturbation Theory and the WKB Methodf�]Sharif Univ of Technology, Dept of Mech Eng, Fax: 98-21-918-23-66, [email protected]?��$,...��e@<���@�<�Mitchell, Jason Wm.��A Simplified Variation of Parameters Formulation of Euler's Equations of Motion of an Arbitrarily Torqued Asymmetric Rigid Body���Univ of Cincinnati, Dept of Aeospace Eng & Eng Mechanics, ML70, Cincinnati, OH 45221-0070, Voice: 513-556-6499 Fax: 513-556-5038, [email protected]��$,...�� e@<���@�<���Lo, Martin W.                       Koon, Wang Sang                           Ross, Shane                       Marsden, Jerrold                    7�.The Genesis Trajectory and Heteroclinic Cyclesf�]Jet Propulsion Lab, California Institute of Technology, 4800 Oak Grove Dr, Pasadena, CA 91109��$,...��@e@<���@�<E�<Ricci, Mario Cesar                     Varotto, Sebastiao C.>�5Development of a Bapta Mechanism for Small Satellites���National Institute for Space Research - INPE, Space Mechanics and Control Division - DMC, CEP 12201-970, Sao Jose dos Campos, Brazil, [email protected]��$,...��`e@<���@<���@�Wnuk, Edwine�\Relation between Osculating and Mean Orbital Elements in the Case of the Second Order Theory���Astronomical Observatory of the A. Mickiewicz Univ, ul.Sloneczna 36, PL-60-286 Poznan, Poland, Voice/Fax: +48(61)8686511, [email protected]��$
Astrodynamics��,...���e@<���@
�< �Viereck, Rodney0�'Solar Maximum Effects on Satellite Drag0�'NOAA Space Environment Lab, Boulder, CO�%�$Atmospheric Density (Marcos)��,...���e@<���@�<F�=Owens, J.                                       Vaughan, W.W.7�.Solar predictions for Space Station Operations_�V(Owens) NASA MSFC (Vaughan) Univ of Alabama, Huntsville, AL, [email protected]�%�$Atmospheric Density (Marcos)��,...���e@<���@�<l�cNicholas, A.C.                             Picone, J.M.                              Thonnard, S.E.{�rA Methodology for Using Optimal MSIS Parameters Retrieved from SSULI Data to Compute Satellite Drag on LEO ObjectsM�DNaval Research Lab, Washington, DC  20375, [email protected]�%�$Atmospheric Density (Marcos)��,...���e@<���@�<���Cefola, Paul                                           Nazarenko, A.                                       Proulx, R.                              Yurasov, V.^�UNeutral Atmosphere Density Monitoring Based on Space Surveillance System Orbital Datad�[The Charles Stark Draper Lab, 555 Technology Square, Cambridge, MA 02139, [email protected]�%�$Atmospheric Density (Marcos)��,...��f@<���@�<9�0Marcos, F.A.                               et alI�@Operational Application of the Atmospheric Calibration Technique �AFRL, [email protected]�%�$Atmospheric Density (Marcos)��,...�� f@<���@�<�Minnow, Joe Dr.j�aTBD - Interested in contributing a paper; likely topic is potential upgrades to empirical models.&�Sverdup, Inc., Huntsville, AL�%�$Atmospheric Density (Marcos)��,...��@f@<���@<���@J�AGlover, Robert A.                         Schumacher, Paul W. Jr.M�DThe Y2K Effort for the Naval Space Command Mission Processing System���(Glover) GRCI, 985 Space Center Drive, #310, Colorado Springs, CO  80915, Voice: 719-596-5395, Fax: 719-596-6139, [email protected] (Schumacher) Naval Space Command, Dahlgren, VA��$,...��`f@<`��@�<Q�HViereck, Rodney                                          Joselyn, Jo AnnM�DThe Solar Cycle and its Effect on Neutral Density and Satellite Drag[�RNOAA Space Environment Lab, 325 Broadway, Boulder, CO 80303, [email protected]�%�$Atmospheric Density (Marcos)��,...���f@<`��@�<>�5Pardini, C.                               Anselmo, L.z�qCalibration of Semi-Empirical Atmosphere Models through the Orbital Decay of Spherical and Cylindrical Satellites7�.[email protected]; [email protected]�%�$Atmospheric Density (Marcos)��,...���f@<`��@�<���Tolson, R.H.                               Keating, G.M.                          Baird, D.T.                           Noll, S.N.                             Shellenberg, T.I.X�OUtilization of Mars Global Surveyor Accelerometer Data for Atmospheric Modeling �[email protected]�%�$Atmospheric Density (Marcos)��,...~
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QActionsUSess 1*_!Mission Design: Mars - Bob Melton�fffffffg	
TMon AM��r@Lb@M���@M���@�N�Cesarone, R.J.                                 Hastrup, R.C.                                    Bell, D.J.                                             Roncoli, R.G.[NRArchitectural Design for a Mars Communications & Navigation Orbital Infrastructure~NuJet Propulsion Lab, California Institute of Technology, 4800 Oak Grove Dr, Pasadena, CA 91109, [email protected]NRIC Abs.docOMission Design~
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��r@@[@< ��@<���@�Kallemeyn, Pieter                            Cangahuala, Alberto                      Ely, Todd; Bell, David                                            Guinn, Joseph                                   Bar-Sever, Yoaz E.                         Lichten, Ste`WConstellation Design for a Mars-Orbiting Satellite Communication and Navigation Networkg^Jet Propulsion Lab, Voice: 818-354-9166, Fax: 818-393-6388, [email protected]MarsNet Abstract.doc?Mission Design~
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;  Willcockson, William H.90Mars Polar Lander Entry Descent & Landing Design��Lockheed Martin Astronautics, S8800, POB 179, Denver, CO 80201, Voice: 303-977-5094, Fax: 303-977-9345, [email protected]>5AIAAAbstractSubmittal.MW.doc; MSPEDLPaperAbstract.docJMission Design~
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��r@�[@< ��@<���@��Johnston, M.D.                               Esposito, P.B.                                  Alwar, V.; Demcak, S.W.                                   Graat, E.J.; Burkhart, P.D.                                   Portock, B.M. NEThe Strategy for the Second Phase of Aerobraking Mars Global Surveyor��Jet Propulsion Lab, California Institute of Technology, 4800 Oak Grove Dr, M/S 264-235, Pasadena, CA 91109, Voice: 818-393-1290, Fax: 818-393-3147, [email protected]MGS-AB2-mdj.doc$Mission Design~
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�s@�]@<���@<���@Guo, Yanping3*Aladdin's Phasing and Mission Orbit Design��The Johns Hopkins Univ, APL, Rm 4-141, 11100 Johns Hopkins Rd, Laurel, MD 20723-6099, Voice: 240-228-7541/443-778-7541, Fax: 240-228-1093/443-778-1093, [email protected]AAS Aug abs.doc$Mission Design~
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�s@\@< ��@<���@��Lee, Wayne J.                                    D'Amario, Louis A.                        Roncoli, Ralph B.                            Smith, John C.I@Mission Design Overview for Mars 2003/2005 Sample Return Mission��Jet Propulsion Lab, California Institute of Technology, MS 264-380, 4800 Oak Grove Dr, Pasadena, CA 91109, Voice: 818-354-8784, Fax: 818-393-2902, [email protected]6-aas99 msr abstract.doc aas99 msr abstract.pdf$Mission Design~
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�	 s@ `@<���@<���@�	�D'Amario, Louis A.                     Bollman, Willard E.                          Lee, Wayne J.                                    Roncoli, Ralph B.                             Smith, John C. S	JMars Orbit Rendevous Strategy for the Mars 2003/2005 Sample Return Mission	�Jet Propulsion Lab, California Institute of Technology, 4800 Oak Grove Dr, MS 301-276, Pasadena, CA 91109, Voice: 818-354-3209, Fax: 818-393-5214, [email protected], [email protected], [email protected], [email protected]$	MSR Rendezvous Abstract.doc	$Mission Design~
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IOptimal Two-Impulse and Three-Impulse Maneuvers for Mars orbit Rendezvoust
kThe Charles Draper Lab, 555 Technology Square, Cambridge, MA 02139, Voice: 617-258-2433, [email protected]

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QCombine with #79�0s@�S@<@��@<@��@i`D'Souza, Christopher N.              Kachmar, Peter S.                         Brand, Timothy J.SJTerminal Rendezvous Analysis and Design for the Mars Sample Return Mission�wThe Charles Stark Draper Lab, 555 Technology Square, Cambridge, MA 02139-1000, Voice: 617--258-2433, [email protected]$Mission Design~
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hEllipso, Inc, 1133 21st St, NW, 8th Floor, Washington, DC, 20036, Voice: 202-466-4488, Fax: 202-466-4493

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��C@<���@<@��@Smith, Robert H.d[An Axiomatic Design Approach Applied to the Problem of Comparing Space System Architectures��NASA Programs, The Aerospace Corp, 2101 NASA Rd One, Bldg 45, Rm 650, Houston, TX 77058, Voice: 281-483-3263, Fax: 281-483-9677, [email protected]$Architecture~
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�J@<��@<��@Palmerini, Giovanni B.5,Guidance Strategies for Satellite Formations��Scuola di Ingegneria Aerospaziale, Universita degli Studi di Roma "la Sapienza" 18, via Eudossiana - 00184 Roma - Italy, Voice: +39.06.44585.334, Fax: +39.06.44585.952, [email protected]$Formation Flying~
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��M@<��@<��@Lang, Thomas J.[RCharacteristics of Crosslinks Between Satellites in Large Symmetric ConstellationsofThe Aerospace Corp, POB 92957, M4/947, LAX, CA 90009-2957, Voice: 310-336-4307, [email protected]$Constellations~
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��N@<��@<Unsuccessful e-mailvmYuan, Jianping                                  Fang, Qun                                           Wei, JuanLCDesign and Analysis of Space Station Based Micro-Satellite Networks��College of Astronautics, Northwestern Polytechnical Univ, Xi'an, 710072, P.R. China, Voice:  (86)29-8493685, Fax: (86) 29-8491000, [email protected]$
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�P@<��@< ��@C:Kantsiper, Brian Dr.                         Drake, Howard;2Using Tessellations for Large Constellation Design��Lockheed Martin Missiles & Space, O:L8-30 (E5-10) 8:102, 1111 Lockheed-Martin Way, Sunnyvale, CA  94089, Voice: 408-756-3973, Fax: 408-743-0699, [email protected]$
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��P@<��@<@��@Chichka, David F.>5Dynamics of Clustered Satellites via Orbital Elements��Univ of California, 38-137 Engineering IV, POB 951597, 420 Westwood Plaza, Box 951597, LAX, CA 90095-1597, Voice: 310-825-2902, Fax: 310-236-2302, [email protected]$Formation Flying~
	@
�@Y@< ��@< ��@riSchaub, Hanspeter                         Vadali, Srinivas R.                           Alfriend, Kyle T.F=Spacecraft Formation Flying Control Using Mean Orbit Elements�~Lisa Willingham, Texas A&M Univ, College Station, TX 77843-3141, Voice: 409-845-3947, Fax: 409-845-6051, [email protected]$Formation Flying~
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�P b@M���@M���@NUlivieri, Carlo`NWThe Multi-Synchronous Technique for Environment Monitoring by a Satellite Constellation�N�Centro di Ricerca Progetto San Marco, Univ of Rome "La Sapienza", Via Salaria 851, 00138 Rome, Italy, Voice: +39-06-8120539, Fax: +39-06-8106351, [email protected]NUlivieri.docO
Constellation~
	@
USess 30_'Attitude Control: Theory - Peter Bainum�```````a	
TMon AM�F@<���@<��@KBBanerjee, Arun K.                             Singhose, William E.JAMomentum Dumping with Vibration Reduction for Flexible Spacecraft�(Banerjee) Consulting Scientist, H1-61/250, Lockheed Martin ATC, Palo Alto, CA 94304, Phone: 650-424-2624, Fax: 650-424-3106, [email protected] (Singhose) Mechanical Engineering Dept, Georgia Institute of Technology, Atlanta, GA 30332, Voice: 650-424$Attitude Control~
	@
��Q@<��@<@��@?6Tsiotras, Panagiotis                      Shen, HaijunKBSatellite Attitude Control and Power Tracking with Momentum Wheels�yGeorgia Institute of Technology, Atlanta, GA 30332-0150, Voice: 404-894-9526, Fax: 404-894-2760, [email protected]$Attitude Control~
	@
�N@<��@<��@vmStevens, H.D.                                    Rodden, J.J.                                      Carrou, S.A8Mass Expulsion Control for Precision Pointing Spacecraft��Space Systems/Loral, 3825 Fabian Way, M/S G76, Palo Alto, CA 94303-4604, Voice: 650-852-4210, Fax: 650-852-4928, [email protected]$Attitude Control~
	@
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< ��Modi, V.J.                                                 Cao, Y.                                             deSilva, C.W.                               Misra, A.K.                                   RIController Design for Space Platform-Based Variable Geometry Manipulators}tThe Univ of British Columbia, 2324 Main Mall, Vancouver, B.C. Canada V6T 1Z4, Voice: 604-822-2914, Fax: 604-822-2403$Attitude Control~
	@
�@U@<���@<��@kbRobertson, Michael                      Singhose, William                           Banerjee, ArunJAInitial Guess Schemes for Generating Deflection-Limiting Commands�(Robertson, Singhose) Dept of Mechanical Engineering, Georgia Institute of Technology, Atlanta, GA 30332, Voice: 404-385-0668, Fax: 404-899-9342, [email protected] (Singhose) Voice: 404-385-0668, Fax: 404-894-9342, [email protected] (Bane
 $Attitude Control~
	@
��X@< ��@< ��@Tanygin, SergeiE<Sensitivity of Spin-Axis Reorientation and Delta-V Maneuvers�xAnalytical Graphics, Inc, 325 Technology Dr, Malvern, PA 19355, Voice: 610-578-1030, Fax: 610-578-1001, [email protected]$Attitude Control~
	@
�P�a@M���@M��@NPark, Sang-YoungqNhThermally-Induced Attitude Vibration Control of a Spacecraft with a Flexible Boom Using Smart StructuresNvNaval Postgraduate School, 699 Dyer Rd, Bldg 245, Monterey, CA 93943-5000, Voice: 408-656-2656, [email protected]NOAttitude Control~
	@
�4@<��@<��@Tsiotras, Panagiotis`WFeasible Trajectory Generation for Underactuated Spacecraft Using Differential Flatness��School of Aerospace Engineering, Georgia Institute of Technology, 270 Ferst Drive, Atlanta, GA  30332-0150, Voice: 404-894-9526, Fax: 404-894-2760, [email protected]$Attitude Control~
	@
�.@;��@;��@vmZhang, Bing                                       Wu, Hongxin                                     Zhang, Hong{rExponential Stabilization of Spacecraft's Angular Velocity with Underactuated Configuration of One-Sided Thrusters�(B. Zhang) Beijing Institute of Control Engineering, POB 2729, Section 36, Beijing 100080, P.R.C., Phone: 86-10-68745370, Fax: 86-10-62543110, [email protected] (Wu) Same address (H. Zhang) Dept of Power, Inner Mongolia Technology University, HuhehaJAttitude Control~
	@
�D86lk�n�Q�r|;�l�]��Q��u��t}�2Oz� �T0@ !�b"�b#�b$���%�&�'�b (Y@b )��*�%+��b,�b�-�.��b/�0��1��� 2;@{ 3�4�5��b6�7��8��b9�{ :� ;�z0<��=���>�0�?� S4 _+Orbit Determination: Missions - Jay Middour� ```````aK
!�!�B@;���@;@��@k!bCarranza, Eric                               Konopliv, Alex                             Ryne, Markj!aLunar Prospector Orbit Determination Uncertainties Using the High Resolution Lunar Gravity Models�!�Jet Propulsion Lab, California Institute of Technology, MS 301-125J, 4800 Oak Grove Drive, Pasadena, CA 91109-8099, [email protected]!
lpxabs.doc%!JOrbit Determination Accuracy~
!	@!
"�"�P@<��@< ��@�"�Jacobson, Robert A.                     Haw, Robert J.                                  McElrath, Tim P.                             Antreasian, Peter G._"VA Comprehensive Orbit Reconstruction for the Galileo Prime Mission in the J2000 System�"�Jet Propulsion Lab, California Institute of Technology, MS 301-150, 4800 Oak Grove Dr, Pasadena, CA 91109-8099, Voice: 818-354-7201, Fax: 818-393-6388, [email protected]""$Orbit Determination~
"	@"
#�#Q@<��@<@��@@#7Ryne, Mark                               Criddle, Kevin3#*Nozomi Cis-Lunar Phase Orbit Determination�#�Jet Propulsion Lab, California Institute of Technology, 4800 Oak Grove Dr, Pasadena, CA 91109-8099, Voice: 818-354-8101, Fax: 818-393-6558, [email protected]##$Orbit Determination~
#	@#
$�$@Z@< ��@< ��@B$9Pickard, Henry                                 Hope, AlanP$GAdaptation of a Spaceborne Geolocation System to an Airborne Experiment`$WNaval Research Lab, 4555 Overlook Ave SW, Washington DC 20375-5355, Voice: 202-767-0432$$$???~
$	@$
%�%�[@< ��@<���@n%eGranholm, George R.                     Proulx, Ronald J.                             Cefola, Paul J.H%?Methods of Orbit Determination for EllipsoTM Sub-Constellations�%�The Charles Stark Draper Lab, MS 70, 555 Technology Square, Cambridge, MA 02139, Voice: 617-258-1559, Fax: 617-565-8674, [email protected]%
ala abstr.doc%?Orbit Determination~
%	@%
&�&�b@<���@<���@&�Lemoine, F.G.                                   Rowlands, D.D.                                 Smith, D.E.; Pavlia, D.E.                                 Chinn, D.S.; Luthcke, S.B.                                            Neumann, G.A.                   D&;Orbit Determination for Mars Global Surveyor during Mapping&�(Lemoine, Rowlands, Smith) Lab for Terrestrial Physics, NASA Goddard Space Flight Center, Code 926, Greenbelt, MD 20771, Voice: 301-614-6109, Fax: 310-614-6099, [email protected] (Pavlia, Chinn, Luthcke) Raytheon ITSS, Greenbelt, MD (Neumann, Zu&&$Orbit Determination~
&	@&
'�'P�d@M���@
'M Y'NPBinning, Patrick W.                  Middour, Jay                    Soyka, MarkZ'NQOrbit Determination Using Space to Ground Differential GPS in NRL's OCEAN Package�'N�Naval Research Lab, 4555 Overlook Ave SW, Washington DC 20375-5355, Voice: 202-767-0432, Fax: 202-404-7516, [email protected]'N'OOrbit Determination~
'	@'
(USess 53(_*Solar Sails and Low Thrust - Claig Kluever�(```````a	(
TMon PM)�);@<@��@<@��@D);Rauwolf, Gerald                           Friedlander, AlanN)ENear-Optimal Solar Sail Trajectories Generated by a Genetic Algorithm�)wSAIC, 1501 Woodfield Rd, #202N, Schaumburg, IL  60173, Voice: 847-330-2524, Fax: 847-330-2522, [email protected]) )$Trajectory Optimization~
)	@)
*�*�S@<@��@<@��@>*5Coverstone-Carroll, Victoria        Prussing, John E.8*/A Technique for Earth Escape Using a Solar Sail�*�Univ of Illinois at Urbana-Champaign, MC-236, 306 Talbot Lab, 104 S. Wright St, Urbana, IL 61801, Voice: 217-333-0678, Fax: 217-244-0720, [email protected]**$Optimization~
*	@*
+�+@S@<@��@<@��@g+^Coverstone-Carroll, Victoria        Powers, Robert B.                        Prussing, John E.H+?Solar Sail Optimal Orbit Transfers to Synchronous Stable Orbits�+�Univ of Illinois at Urbana-Champaign, MC-236, 306 Talbot Lab, 104 S. Wright St, Urbana, IL 61801, Voice: 217-333-0678, Fax: 217-244-0720, [email protected] (Prussing) Voice: 217-333-8231++$Optimization~
+	@+
,�,6@<��@<��@,van de Kolk, ChristelG,>Stability of Levitated Cylindrical Orbits by Using Solar Sails�,�Univ of Tennessee Space Institute, MS 26, 411 B.H. Goetheet Parkway, Tullahoma, TN  37388-9700, Voice: 931-393-7103, [email protected],!,$Astrodynamics Solar Sail~
,	@,
-�-P�c@M��@M��@-NSauer, Carl G., Jr.H-N?Solar Sail Trajectories for Solar Polar and Heliopause Missions�-N�Jet Propulsion Lab, California Institute of Technology, MS 301-140H, 4800 Oak Grove Dr, Pasadena, CA 91109, Voice: 818-354-4875, Fax: 818-393-9900, [email protected]-N-O
Solar Sail~
-	@-
.�.�@@<`��@<@��@n.ePetropoulos, Anastassios E.         Longuski, James M.                         Vinh, Nguyen X.       \.SAnalytic Representations of Low-Thrust Trajectories for Gravity-Assist Applications�.�Purdue Univ, 1282 Grissom Hall, West Lafayette, IN 47907-1282, Voice: 765-494-5139, Fax: 765-494-0307, Home Voice: 765-423-1287, [email protected] (Vinh) Univ of Michigan.1.$(Trajectory Optimization, Relative Motion~
.	@.
/�/@P@<��@< ��@M/DSims, Jon A.                                      Flanagan, Steve N.A/8Preliminary Design of Low-Thrust Interplanetary Missions�/�Jet Propulsion Lab, California Institute of Technology, MS 301-142, 4800 Oak Grove Dr, Pasadena, CA 91109-8099, Voice:  818-354-0313, Fax: 818-393-9900, [email protected]//$Mission Design~
/	@/
0�0�T@<���@<��@A08Colasurdo, Guido                       Casalino, LorenzoP0GTrajectories towards Near-Earth-Objects Using Solar Electric Propulsion�0�Dipartimento di Energetica - Politecnico di Torino C.so Duca degli Abruzzi 24, 10129 Torino, Italy, Voice: +39-011-564-4426, Fax: +39-011-564-4599, [email protected]00$Optimization~
0	@0
1�1 @; ��@
1; ;12Guelman, Mauricio                        Tahan, D.d1[Solar Electric Propulsion Earth to Mercury Optimal Trajectories with Variable Maximum Power�1�Facility of Aerospace Engineering, Israel Institute of Technology, Technion City, Haifa, 32000, Israel, Voice: 972-4-829-3020, Fax: 972-4-823-0956, [email protected]11JMission Design~
1	@1
2S.2_%Topics in Control Theory - Tom Carter�2```````aK
3�3E@;���@;@��@�3�Bedrossian, Nazareth                            Jang, Jiann-Woei                              Watson, James                     Grigoriadis, KarolosX3OReducing Conservatism of Analytic Transient Response Bounds via Shaping Filters�3�The Charles Stark Draper Lab, 2200 Space Park Dr, #210, Houston, TX 77058, Voice: 281-333-2127, Fax: 281-333-5276, [email protected]3Shaping.doc3JAttitude Theory~
3	@3
4�4V@<���@<��@}4tWie, Bong                                          Lu, Jianbo                                          Bailey, DavidM4DNonlinear Feedback Control Logic for Jerk-Free, Rapid Slew Maneuvers�4�(Wie, Lu) Arizona State Univ, Tempe, AZ 85287-6106, Voice: 602-965-8674, Fax: 602-965-1384, [email protected] (Bailey) Satellite Systems Operation, Honeywell Inc., Glendale, AZ 85308-965044$Attitude Control~
4	@4
5�5�^@<���@<���@C5:Longman, Richard W.                         Chen, Hong-JenY5PImproved Performance of Repetitive Controllers using Smoothing of Control Inputs�5�Columbia Univ, MS 4703, Rm 220, Mudd Bldg, 500 West 120th St, New York, NY 10027, Voice: 212-854-2959, Secretary#: 212-854-2965, [email protected]55$Control, Robots~
5	@5
6�6�^@<���@<���@q6hLongman, Richard W.                         Giese, Guido                                  Bock, H. GeorgQ6HThe Optimized Interaction Forces in Minimum Time Control of Elbow Robots6�(Longman) Columbia Univ, MS 4703, Rm 220, Mudd Bldg, 500 West 120th St, NY, NY 10027, Voice: 212-854-2959, Secretary#: 212-854-2965, [email protected] (Giese) Swiss Federal Institute of Technology Zurich (ETH), Zurich, Switzerland (Bock) Univ of Heidelber66$Control, Robots~
6	@6
7�7_@<���@<���@?76Longman, Richard W.                     Plotnik, Aarong7^Subtleties in the Use of Zero-Phase Low-Pass Filtering and Cliff Filtering in Learning Control�7�(Longman) Columbia Univ, MS 4703, Rm 220, Mudd Bldg, 500 West 120th St, NY, NY 10027, Voice: 212-854-2959, Secretary#: 212-854-2965, [email protected] (Plotnik) Allied Signals, Inc, Teterboro, NJ77$Control ~
7	@7
8�8 a@<���@<��@�8�Carter, Scott Capt.                         McLaughlin, Craig Dr.                    Sabol, Chris Dr.                                Bir, Megan Lt.]8TSpaceflight Dynamics Support for the MightySat II.1 Hyperspectral Payload Operations8�(Carter) Air Force Research Lab/VSSS, 3550 Aberdeen Ave SE, Kirtland AFB, NM 87117-5718, Voice: 505-853-3970, Fax: 505-846-0033, [email protected] (McLaughlin) Voice: 505-853-6545, Fax: 505-846-6053, [email protected] (Sabol) Voice: 505-846-4056, Fax: 88$Mission Control~
8	@8
9�9P@e@M���@9ME9N<Ricci, Mario Cesar                     Varotto, Sebastiao C.>9N5Development of a Bapta Mechanism for Small Satellites�9N�National Institute for Space Research - INPE, Space Mechanics and Control Division - DMC, CEP 12201-970, Sao Jose dos Campos, Brazil, [email protected]�
9NO~
9	@9
:S7:_.Launch and Mission Support Tools - Les Scakett�:```````aK
;�;�?;��@;@��@;Turner, Andrew E.R;IAquarius, a Low-Cost, Low-Reliability Launch Vehicle to Carry Consumables�;�Orbit Dynamics Section, Space Systems/LORAL, MS G-76, 3825 Fabian Way, Palo Alto, CA  94303, Voice: 650-852-407, Fax: 650-852-4666, [email protected];;JLaunch Vehicle~
;	@;
<�<�W@<��@< ��@<Slane, Frederick A.D<;The Importance of Space Standards: An Astrodynamics Example<[email protected]<<$	Standards~
<	@<
=�=�\@<���@<���@J=AHack, Kurt J.                                      Riehl, John P.P=GTrajectory Development and Optimization of an RBCC-based Launch Vehicle�=�(Hack) NASA, John Glenn Research Center at Lewis Field, 2100 Brookpark Rd, MS 500-201, Cleveland, OH, Voice: 216-977-7060, Fax: 216-977-7125, [email protected] (Riehl) Voice: -7061, [email protected]=%=$Launch Vehicle, Optimization~
=	@=
>�>�\@<���@<���@y>pHarsch, Jenna                                  Middour, Jay                                     Llewellyn, Robin@>7Orbit Analysis Tools Software (Version 1 for WindowsTM)�>~U.S. Naval Research Lab, 4555 Overlook Ave SW, Washington DC, Voice: 202-767-6509, Fax: 202-404-7516, [email protected]>>$Mission Design, Tools~
>	@>
?�?�`@<���@<��@@?7Woodburn, James                          Ohlarik, Deronj?aA Graphical Method for the Computation of Antenna Obscuration for the International Space Station�?xAnalytical Grahpics, Inc, 325 Technology Dr, Malvern, PA 19335, Voice: 610-578-1000, Fax: 610-578-1001, [email protected]??$
Astrodynamics~
?	@?
�D�5l^�-�V���w���m����X���:�q}a}���@�T0A�b Bb C�bD���E�F�G�bH�bI��J�%K��b Lb� M�N��bO�P��Q���R�{S�T�U��b V W��X��bY�{Z��[�z0\��]���^�0�_� @�@�`@<���@<��@J@AGist, Robert G.                                  Oltrogge, Danieln@eCollision Vision: Covariance Modeling and Intersection Detection for Spacecraft Situational Awareness�@�The Aerospace Corp, POB 92957, M4/946, LAX, CA 90009-2957, Voice: 310-336-4297, Fax: 310-336-5827, [email protected] (Oltrogge) Voice: 719-554-6026, Fax: 719-554-5876, [email protected]@@$Close Approach~
@	@@
A�AL@f@M���@M���@JANAGlover, Robert A.                         Schumacher, Paul W. Jr.MANDThe Y2K Effort for the Naval Space Command Mission Processing System�AN�(Glover) GRCI, 985 Space Center Drive, #310, Colorado Springs, CO  80915, Voice: 719-596-5395, Fax: 719-596-6139, [email protected] (Schumacher) Naval Space Command, Dahlgren, VA�
ANO~
A	@A
BS/B_&Mission Design: Planets - Lou D'Amario�B```````aK
C�C�A@;`��@;@��@�CBonfiglio, Eugene P.                        Longuski, James M.                                Vinh, N.X.                       <C3Automated Design of Aerogravity-Assist Trajectories�C�Purdue Univ, 1282 Grissom Hall, West Lafayette, IN 47907-1282, Voice: 765-494-5139, Fax: 765-494-0307, Home Voice: 765-423-1287, [email protected] (Vinh) Univ of MichiganC"CJAerogravity, Optimization~
C	 @C
D�D�Y@< ��@< ��@DMcRonald, Angus D.JDAA Light-Weight Inflatable Hypersonic..Drag Device for Venus Entry8D/Jet Propulsion Lab, [email protected]D D$Reentry, Mission Design~
D	 @D
E�E�Y@< ��@< ��@�E�Wilson, M.G.                                      Johannesen, J.R.                             Halsell, C.A.                                      Haw, R.J.                                             Pojman, J.L.:E1Post Galileo-Europa-Mission Satellite Tour Design�E�Jet Propulsion Lab, California Institute of Technology, M/S 301-276, 4800 Oak Grove Dr, Pasadena, CA 91109-8099, Voice: 818-354-2567, Fax: 818-393-5214, [email protected]EE$Mission Design~
E	 @E
F�F�`@<���@<��@FLyons, Daniel T. Dr.pFgAerobraking at Venus and Mars: A Comparison of the Magellan and Mars Global Surveyor Aerobraking Phases�F�Jet Propulsion Lab, California Institute of Technology, Pasadena,  CA 91109, Voice: 818-393-1004, Fax: 818-393-3147 [email protected]FF$Aerobraking~
F	 @F
G�G�a@<���@<��@�G�Esposito, P.B.; Alwar, V.                                               Burkhart, P.D.; Demcak, S.W.                                   Graat, E.J.; Johnston, M.                                                       Portock, B.M. VGMNavigating Mars Global Surveyor through the Martian Atmosphere: Aerobraking 2�G�Jet Propulsion Lab, California Institute of Technology, 4800 Oak Grove Dr, Pasadena, CA 91109, Voice: 818-393-1264, Fax: 818-393-3147, [email protected]GG$Aerobraking~
G	 @G
H�H�a@<���@<���@BH9Johannesen, Jennie R.                  D'Amario, Louis A.1H(Europa Orbiter Mission Trajectory Design�HzJet Propulsion Lab, California Institute of Technology, 4800 Oak Grove Dr, Pasadena, CA 91109, [email protected]'HAbst AAS 99 Europa Orbiter.docH$Mission Design~
H	 @H
I�I�c@<��@<��@IPenzo, Paul A.AI8Venus and Beyond Using the Ariane ASAP Launch Capability�I�Jet Propulsion Lab, California Institute of Technology, MS 301-140H, 4800 Oak Grove Dr, Pasadena, CA 91109, Voice: 626-354-6162, Fax: 626-393-9900, [email protected]I'I$Launch Vehicle, Mission Design~
I	 @I
J�J d@<@��@<`��@�J�Sweetser, Ted                          Cameron, Jonathon              Chen, Gun-Shing                     Cuts, Jim; Gershman, Bob, Gilmore, Martha S.               +10 other authors                                                GJ>Venus Surface Sample Return: A Weighty High-Pressure Challenge�JxJet Propulsion Lab, California Institute of Technology, 4800 Oak Grove Dr, Pasadena, CA 91109, [email protected]JVSSR.pdfJ$Mission Design~
J	 @J
K�KP�d@M@��@M@��@KNMatousek, SteveNKNESpaceTime - A MIDEX Proposal to Test Einstein's Equivalence Principle�KN�Jet Propulsion Lab, California Institute of Technology, MS 264-426, 4800 Oak Grove Dr, Pasadena, CA 91109, Voice: 818-354-6689, Fax: 818-393-6800, [email protected]#KNAug 99 AK abs-Matousek.pdfKO~
K	 @K
LS*L_!Orbit Determination - David Cicci�L```````aK
M�M,@;���@
M; MSrinivasan, B.�M�Orbit Determination of Geo-Stationary Satellites Using a Parabolic Sinusoidal Fit for Longitude and a Sinusoidal Fit for the Sine of Declination�M~INSAT-Master Control Facility, Dept of Space, Government of India, Hassan-573201, Karnataka State, India, Fax: 0091-8172-67423MMJOrbit Determination~
M	"@M
N�ND@<���@<@��@�N�Danielson, Don A.                          Canright, D.                              Perini, Deborah, N.                     Schumacher, Paul W.JNAThe Naval Space Command Automatic Differential Correction Process�N�(Danielson/Canright) Dept of Mathematics, Code MA/Dd, Rm Glasgow 341, Naval Postgraduate School, Monterey, CA 93943-5216, Voice: 831-656-2622, Fax: 831-656-2355, [email protected] (Perini/Schumacher) Naval Space Command, Dahlgren, VA 22448 NAAS.docN$Orbit Determination~
N	"@N
O�O�U@<���@O<Unsuccessful e-mailtOkMcLaughlin, Craig A.                     Gold, Kenn                                         Born, George H.;O2Altitude Effects on Autonomous Orbit Determination�O�(McLaughlin) Air Force Research Lab/VSSS, 3550 Aberdeen Ave., SE, Kirtland AFB, NM 87117-5718, Voice: 505-853-6545, Fax: 505-846-6053, [email protected] (Gold, Born) Univ of Colorado, Campus Box 428, Boulder, CO 80309-0428, Voice: 303-492-8638OO$Drag Modelling?~
O	"@O
P�P@^@<���@<���@FP=Alfriend, Kyle T.                                Lim, Jong-IlNPEPerformance of a Dynamic Algorithm for Processing Uncorrelated Tracks�P}Texas A&M Univ, H.R. Bright Bldg, Rm 701, College Station, TX, Voice: 409-845-5920, Fax: 409-845-6051, [email protected]PAnchorage-Abstract.docP$
Astrodynamics~
P	"@P
Q�Q@_@<���@<���@�Q�Gabor, Michael J.                     Nerem, R. Steven                                                                                                               \QSGPS Carrier Phase Ambiguity Resolution Using Satellite-Satellite Single Differences�Q�(Gabor) AFRL and Univ of Texas Center for Space, [email protected] (Nerem) Univ of Texas Center for Space Research, [email protected]          Qabs.psQ$???~
Q	"@Q
R�R``@<���@<���@RPowell, Thomas D.\RSAutomated Tuning of an Extended Kalman Filter using the Downhill Sismplex Algorithm�R{The Aerospace Corp, POB 92957, M4/962, LAX, CA 90009-2957, Voice: 310-336-5572, Fax: 310-336-1812, [email protected]RR$Orbit Determination~
R	"@R
S�Sa@<���@<��@rSiBir, Megan Lt.                                   Carter, Scott Capt.                         Sabol, ChrisbSYParametric Analysis for the Selection of Data Source in the Orbit Determination ProcessesS�(Bir) Air Force Research Lab/VSSS, 3550 Aberdeen Ave SE, Kirtland AFB, NM 87117-5718, Voice: 505-853-4136, Fax: 505-846-6053, [email protected] (Carter) Voice: 505-853-3970, Fax: 505-846-0033, [email protected] (Sabol) Voice: 505-846-4056, Fax: 50SS$Orbit Determination~
S	"@S
T�T@a@<���@<��@�T�Carter, Scott Capt.                         Sabol, Chris Dr.                                Burns, Richard                                 Bir, Megan Lt.8T/A Fresh Look at Angles-Only Orbit DeterminationT�(Carter) Air Force Research Lab/VSSS, 3550 Aberdeen Ave, SE, Kirtland AFB, NM 87117-5718, Voice: 505-853-3970, Fax: 505-846-0033, [email protected] (Sabol) Voice: 505-846-4056, Fax: 505-846-6053, [email protected] (Burns) Voice: 505-846-2352, Fax: 505-84TT$
Astrodynamics~
T	"@T
U�UP�a@M���@M���@LUNCCurti, F.                                               Parisse, M.>UN5Low Earth Orbit Estimation from Single Ground Station�UN�Centro di Ricerca Progetto San Marco, Univ of Rome "La Sapienza", Via Salaria 851, 00138 Rome, Italy, Voice: +39-06-8120530, Fax: +39-06-8105241, [email protected]UN	CURTI.docUOOrbit Determination~
U	"@U
VSAV_8Attitude Dynamics and Control: Applications - Chris Hall�V```````aK
W�WC@;���@;@��@�W�Hall, Robert A.                             Kirchwey, Kim                             Martin, Michael                           Rosch, Gene                                 Zimpfer, DouglasSWJFlight Control Overview of STS-88, the First Space Station Assembly Flight�W�The Charles Stark Draper Lab, 2200 Space Park Dr, #210, Houston, TX 77058, Voice: 281-333-2198, Fax: 281-333-5276, [email protected]WHall_AAS.docWJAttitude Control~
W	$@W
X�X�D@<���@<@��@XBedrossian, NazarethAX8Space Station Attitude Control During Payload Operations�X�The Charles Stark Draper Lab, 2200 Space Park Dr, #210, Houston, TX 77058, Voice: 281-333-2127, Fax: 281-333-5276, [email protected]XX$Attitude Control~
X	$@X
Y�Y@V@<���@Y<Unsuccessful e-mailHY?Fonseca, Ijar M.                              Bainum, Peter M. �Y�Integrated Structural and Control Optimization of a Large Space Structure Subject to the Gravity-Gradient Torque by Using Analytical Sensitivity Analysis�Y�(Fonseca) National Institute for Space Research - INPE, 12223-970 S.J. Campos, S.P., Brazil, Voice: 55-12-329-7242, [email protected] (Bainum) Howard Univ, 2300 6th Street, NW, Washington DC, 20059, Voice: 202-806-6612, [email protected]YY$Attitude Control~
Y	$@Y
Z�Z`b@<���@<���@tZkHarvie, Edwin                                    Phenneger, Milt                               Dress, AndreZZQMagnetic Precession Attitude Dynamics for On-Orbit Storage of the GOES SpacecraftZ�(Harvie) ASRC Aerospace, 6411 Ivy Ln, #610, Greenbelt, MD 20770, Voice: 301-345-4500 X229, Fax: 301-345-9274, [email protected] (Phenneger) X231, [email protected] (Dress) NOAA, Dept of Commerce, FOB#4, Suitland, MD 20746, Voice: 301-457-5ZZ$Attitude Control~
Z	$@Z
QCombine with # 152[�[�b@<���@<���@r[iToniolo, Matthew D.                      Lee, Mokin                                         Gray, Gary L.�[�Comparison of Melnikov's Method and Numerical Simulation for Predicting Nonlinear Dynamics in the Pitch Motion of Actively Controlled Satellites in a Gravity Gradient Field�[�The Pennsylvania State Univ, 227 Hammond Bldg, Univ Park, PA 16802-1401, Voice: 814-865-4523, Fax: 814-863-7967, [email protected][[$Attitude Theory~
[	$@[
\�\c@<���@<��@l\cDress, Andre                               Harvie, Edwin                            Phenneger, Milt[\RControl Methods for the Activation and Operation of the GOES On-Orbit Storage Mode\�(Dress) NOAA, Dept of Commerce, FOB#4, Suitland, MD 20746, Voice: 301-457-5180 X196, Fax: 301-457-5175, [email protected] (Harvie) ASRC Aerospace, 6411 Ivy Ln, #610, Greenbelt, MD 20770, Voice: 301-345-4500 X229, Fax: 301-345-9274, edwin.harvie@akspaN\EStorage Control Abstract(1).doc;      Storage Control Abstract(1).txt\$Attitude Control~
\	$@\
QCombine with #147]�]`c@<��@<��@�]�Kubitschek, Daniel G.              Gold, Kenneth                         Ondrey, Michael                      Axelrad, Penina                        Born, George H.P]GICESat Attitude Algorithm for Maintained Reference Groundtrack Pointing�]�Univ of Colorado, Campus Box 431, Boulder, CO 80309-0431, Voice: 303-492-6677, Fax: 303-492-2825, [email protected]]]$Attitude Control~
]	$@]
^�^@d@<`��@<`��@l^cde Lafontaine, Jean               Vuilleumier, Pierrik                 Van den Braembussche, Pieter3^*Autonomous Control of the Proba Spacecraft^�(Jean) Universite de Sherbrooke, 2500, boul de l'Universite, Sherbrooke, (Quebec), J1K 2R1, Canada, [email protected] (Pierrik) ESA/ESTEC, Keplerlaan 1, 2201 AZ Noordwijk, the Netherlands (Pieter) Verhaert Design and Development nv, Hogenakk!^AAS AIAA Astrod Conf.doc^$
Navigation~
^	$@^
_�_L�d@M��@M��@_NMackison, Donald L.1_N(ATTDES - Generalized Equations of Motion�_N|Univ of Colorado, Campus Box 429, Boulder, CO 80309-0429, Voice: 303-492-6417, Fax: 303-492-7881, [email protected]_Nastro99-abstract.doc _OAttitude Control, Tools~
_	$@_
�D�;l��Y�?�`��1�T�Y7�nPP�k#Yo\"��-`hT0@ a�bb�bc�bd���e�f�g�bh�bi�� j% k��bl�b�m�n��bo�p��q���r�{ sh@ t�@u��@bv�@w��@xW�@by�{z�� {Yz0@ |��}���~�0��`S=`_4Special Session: Atmospheric Modeling - Frank Marcos�````````aK
a�a@;���@;��@;a2Pardini, C.                            Anselmo, L.zaqCalibration of Semi-Empirical Atmosphere Models through the Orbital Decay of Spherical and Cylindrical Satellites�a�CNUCE, via S. Maria 36, I-56126 Pisa, Italy, Fax: +39-050-904052 (Pardini), Voice: +39-050-593328, [email protected] (Anselmo), Voice: +39-050-593220, [email protected]XaOAAS99_abs.doc;                                                 odea.ps; odee.psaJAtmopsheric Modeling~
a	&@a
b�b?@<`��@b< 2/19/99pbgNicholas, A.C.                              Picone, J.M.                                 Thonnard, S.E.{brA Methodology for using optimal MSIS Parameters Retrieved from SSULI Data to Compute Satellite Drag on LEO Objects�b�(Nicholas) Naval Research Lab, Code 7623, 4555 Overlook Ave, Washington, DC 20375, Voice: 202-767-2441, Fax: 202-767-9388, [email protected] (Thonnardj) Code 7623 (Picone) Code 7643bb$Atmopsheric Modeling~
b	&@b
c�c�G@<���@<��@�c�Tolson, R.H.                                     Keating, G.M.                                    Baird, D.T.                                          Noll, S.N.                                             Shellenberg, T.I.XcOUtilization of Mars Global Surveyor Accelerometer Data for Atmospheric Modelingc�George Washington Univ, Joint Institute for the Advancement of Flight Sciences, Langley Research Center, MS 269, Hampton, VA 23681-2199, Voice: 804-864-1982, Fax: 804-864-5894, [email protected], (Home) 7505 River Road, Apt. PE, Newport News, VA 236cc$Atmospheric Modeling~
c	&@c
d�d�e@<���@
d< dViereck, Rodney0d'Solar Maximum Effects on Satellite Drag0d'NOAA Space Environment Lab, Boulder, COd%d$Atmospheric Density (Marcos)~
d	&@d
e�e�e@<���@e<Fe=Owens, J.                                       Vaughan, W.W.7e.Solar predictions for Space Station Operations_eV(Owens) NASA MSFC (Vaughan) Univ of Alabama, Huntsville, AL, [email protected]e%e$Atmospheric Density (Marcos)~
e	&@e
f�f�e@<���@f<�f�Cefola, Paul                                           Nazarenko, A.                                       Proulx, R.                              Yurasov, V.^fUNeutral Atmosphere Density Monitoring Based on Space Surveillance System Orbital Datadf[The Charles Stark Draper Lab, 555 Technology Square, Cambridge, MA 02139, [email protected]f%f$Atmospheric Density (Marcos)~
f	&@f
g�gf@<���@g<9g0Marcos, F.A.                               et alIg@Operational Application of the Atmospheric Calibration Technique gAFRL, [email protected]g%g$Atmospheric Density (Marcos)~
g	&@g
h�h f@<���@h<hMinnow, Joe Dr.jhaTBD - Interested in contributing a paper; likely topic is potential upgrades to empirical models.&hSverdup, Inc., Huntsville, ALh%h$Atmospheric Density (Marcos)~
h	&@h
i�iL`f@M`��@iMQiNHViereck, Rodney                                          Joselyn, Jo AnnMiNDThe Solar Cycle and its Effect on Neutral Density and Satellite Drag[iNRNOAA Space Environment Lab, 325 Broadway, Boulder, CO 80303, [email protected]iN%iOAtmospheric Density (Marcos)~
i	&@i
jUSess 12;j_2Stationkeeping and Proximity Operations - Todd Ely�j```````a	j
TTues PMk�k(@;���@;���@�k�Smith, James E., 2LT, USAF                     Proulx, Ronald J.                    Cefola, Paul J.                        Draim, John E.wknAn Operational Approach for Generating Near-Optimal Station Keeping Strategies via Parallel Genetic Algorithms�k�The Charles Stark Draper Lab Fellow, AFIT/CIGG-DET 365, MIT, 555 Technology Square, MS 70, Cambridge, MA  02139, Voice: 617-258-2094, Fax: 617-258-2772, [email protected]akXAlaska abstract cover letter1.doc;                                   Alaska Abstract.dockJStationkeeping~
k	(@k
l�l0@<��@<��@klbKamel, Ahmed, Dr.                      Gelon, Walter                               Reckdahl, KeithPlGA Practical Stationkeeping Method for Modular Geosynchronous Satellites�l�Space Systems/LORAL, MS Z01, 3825 Fabian Way, Palo Alto, CA  94303-4604, Voice: 650-852-6197, Fax: 650-852-4661, [email protected]ll$Stationkeeping~
l	(@l
m�m@@<`��@<@��@mEly, Todd A., Dr.WmNImpact of Eccentricity on East-West Stationkeeping for the GPS Class of Orbits�m�Jet Propulsion Lab, California Institute of Technology, 4800 Oak Grove Drive, MS 301-125L, Pasadena, CA 91109-8099, Voice: 818-393-1744, Fax: 818-393-6388, [email protected]mm$Stationkeeping~
m	(@m
n�nG@<���@<��@Hn?Martinot, V.                                       Vignaux, D. _nVEarth-Centered Angle Station-Keeping in Low-Earth Orbits with Yaw-Steering Constraintsn�(Martinot) Departement Missions et Performances des Systemes, Service Performances Operationnelles, Voice: 05-34-35-65-16, Fax: 05-34-35-61-63, [email protected] (Vignaux) Voice: +33-5-6119-4508, Fax: +33-5-6119-6163, david.vignaux.alcatelnGirdwood_abs1.docn$Stationkeeping~
n	(@n
o�oL@]@M���@M���@EoN<Demarest, P.                                    Schutz, B.E.<oN3Maintenance of the ICESat Exact Repeat Ground Track�oN�(Demarest) Univ of Texas at Austin, 3925 W. Braker Ln, #200, Austin, TX 78759-5321, Voice: 512-471-5509, Fax: 512-471-3570, [email protected] (Schutz) Voice: 512-471-4267, Fax: Same, [email protected]oNoO
Astrodynamics~
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p�pO@<��@<��@wpnDou, Xiaomu                                     Huang, Ying                                       Luo, JianjunAp8Orbit Analysis of the Adjoint Satellite to Space Station�p�College of Astronautics, Northwestern Polytechnical Univ, 710072, Xi'an, P.R. China, Voice:  (86)29-8493685, Fax: (86)29-8491000, [email protected]p(p$Relative Motion, Stationkeeping~
p	(@p
q�q<@<@��@<@��@qWright, James R. 5q,Close Approach Spacecraft Maneuver Criterion�q�Analytical Graphics, Inc, Voice: 610-578-1095, [email protected] (Home) POB 647, Morgantown, PA 19543, Voice: 610-286-1795, Fax: 610-286-4798q(q$Close Approach, Relative Motion~
q	(@q
r�r9@< ��@<@��@rAdamo, Daniel R.[rRContingency ISS Rendezvous Recovery Planning by Houston and Moscow Control CentersvrmMacMission Control, 4203 Moonlight Shadow Court, Houston, TX 77059-5525, Voice: 281-480-9631, [email protected]rJUReAbstract.doc!r$Optimization, Rendezvous~
r	(@r
sSRs_IMission Design: Near Earth, Earth/Moon, and Libration Points - Dave Folta�s```````aK
t0�t7@; ��@;@��@�t�Williams, Kenneth E.                   Hong, Philip E.                             Zietz, Richard P.                          Han, DonCt:Maneuver Design and Calibration for the Genesis Spacecraft�t�Jet Propulsion Lab, Navigation and Flight Mechanics Section, California Institute of Technology, 4800, Oak Grove Drive, Pasadena, CA 91109-8099, Voice: 818-354-8132, Fax: 818-393-6388, [email protected]ttJMission Design~
t	0*@t
u0�uR@< ��@<@��@�u�Folta, David                                 Beckman, Mark                          Lozier, David                            Galal, Ken�u�The Lunar Prospector Mission: Final Results of Trajectory Design, Quasi-Frozen Orbits, Extended Mission Targeting, and the Lunar Topography and Potential Models�u�(Folta/Beckman) NASA Goddard Space Flight Center, Code 571, Greenbelt, MD 20771, Voice: 301-286-6082, Fax: 301-286-1719, [email protected] (Lozier/Galal) Ames Research Center, NASAuLunarPro.docu$Mission Design~
u	0*@u
v0�vW@<��@<��@gv^Wilson, R.S.                                 Howell, Kathleen C.                      Lo, M.W.[vROptimization of Insertion Cost for Transfer Trajectories to Libration Point Orbits�v�(Wilson & Lo) Jet Propulsion Lab, California Institute of Technology, 4800 Oak Grove Dr, Pasadena, CA 91109-8099 (Howell) School of Aeronautics & Astronautics, Purdue Univ, 1282 Grissom Hall, West Lafayette, IN  47907-1282v$v$Optimization, Astrodynamics~
v	0*@v
w0�w�X@< ��@< ��@wwnMullins, Larry D.                               Stone, Russell L.                             Evans, Steven W.;w2Mission Planning for the CHANDRA X-ray Observatory�w}Marshall Space Flight Center, ED13, Huntsville, AL 35812, Voice: 256-544-2278, Fax: 256-544-5416, [email protected]wCHANDRA_Abstract.docw$Mission Design~
w	0*@w
x0�x�c@<��@<��@xChern, Jeng-ShingDx;System Design Considerations for a Formosa-X Microsatellite}xtChung Shan Institute of Science and Technology, POB 90008-6-7, Lungtan, Taiwan 32526, R.O.C., [email protected]x	AAS02.docx$Mission Design~
x	0*@x
y0�y�c@<��@<`��@�yxBell, Julia L.                               Lo, Martin W.                                               Wilson, Roby S."yGenesis Trajectory DesignyvJet Propulsion Lab, California Institute of Technology, 4800 Oak Grove Dr, Pasadena, CA 91109, [email protected]yy$Mission Design~
y	0*@y
z0�zPd@M��@M`��@<zN3Beckman, Mark                       Guzman, Jose J.zNTriana Mission DesignzN�(Beckman) Goddard Space Flight Center, Code 572, Greenbelt, MD 20771, Voice: 301-286-8866, Fax: 301-286-0369, [email protected] (Guzman) Purdue Univ, Grissom Hall 1282, West Lafayette, IN 47907-1282, Voice: 765-494-5132, Fax: 765-494-0307, jguzmazNzOMission Design~
z	0*@z
{S.{_%Trajectory Optimization - John Hanson�{```````aK
|�|@;���@|;Unsuccessful e-mail|
Yan, Hui, Dr.L|COptimal Low-Thrust Earth-Moon Targeting Strategy for N-Body ProbleM|�(thru 3/12/99) POB 2729, Beijing, 100080, China, Voice: 0086-010-68745370, Fax: 0086-010-62543110, [email protected] (after 3/12/99) Dept of Aero. & Astronautics, Code AA/Yh, Naval Postgraduate School, 699 Dyer Rd, Monterey, CA 93943, Voice: 8| |JTrajectory Optimization~
|	,@|
}�}@<��@<��@{}rAntonio Fernando Bertachini de Almeida Prado; Maria Matilde Netto dos Santos Paulo; Marcelo Lopes Oliveira e Souza=}4Numerical Research in Non-Coplanar Orbital Maneuvers}�(Prado) Instituto Nacional de Pesquisas Espaciaia - Sao Jose dos Campos - SP - 12227-010, Voice: 55-12-3456201, Fax: 55-12-3456226, [email protected] (Paulo) CDT-ETEP - Av.Barao do Rio Branco 882 - Sao Jose dos Campos - SP - 12242-800 (Souza) Same as Prad}aasabsprado.doc }$Trajectory Optimization~
}	,@}
~�~$@<@��@<`��@~Kechichian, Jean A.z~qThe Optimization of Continuous Constant Acceleration Transfer Trajectories in the Presence of the J2 Perturbation�~{The Aerospace Corp, MS M4/947, POB 92957, LAX, CA 90009, Voice: 310-336-1422, Fax: 310-336-5827, [email protected]~~$Optimization~
~	,@~
�5@<��@
< Carter, Thomas E.lcNecessary and Sufficient Conditions for Optimal Impulsive Rendezvous and Linear Equations of MotionriEastern Connecticut State Univ, Math/CSC Dept, 83 Windham St, Willimantic, CT  06226, Voice: 860-465-5000!$Optimization, Rendezvous~
	,@
�Dt6lg75��]�#)z����2��cv||%�V��X�J���T0��b��b��b���� � ����b��b�����%���b��b� � ���b�����������{�������b � ������b��{�����z0���������0@���@ ����J@<��@<��@�Human, Mel C�:Generalized Planetary Reentry Minimal Heating Trajectories��North Carolina A&T State Univ, 1601 East Market St, Greensboro, NC 27411, Voice: 336-334-7620, Fax:336-334-7417, [email protected]��$Optimization~
�	,@�
����T@<���@<��@A�8Colasurdo, Guido                       Casalino, Lorenzo^�UOptimal DeltaV-Earth-Gravity-Assist Trajectories in the Restricted Three-Body Problem���Dipartimento di Energetica - Politecnico di Torino C.so Duca degli Abruzzi 24, 10129 Torino, Italy, Voice: +39-011-564-4426, Fax: +39-011-564-4599, [email protected]��$Optimization~
�	,@�
���Y@< ��@< ��@E�<Gefert, Leon P.                                Hack, Kurt J.w�nLow-Thrust Control Law Development for Transfer from Low Earth Orbits to High Energy Elliptical Parking Orbits���(Gefert) NASA , John Glenn Research Center at Lewis Field, 21000 Brookpark Rd, MS 500-201, Cleveland, OH, Voice: 216-977-7117, Fax: 216-977-7125, [email protected] (Hack) Voice: 216-977-7060, [email protected]��$Optimization~
�	,@�
���@\@<`��@<���@�Ross, I, Michael5�,Thrust Programming in Aeroassisted Maneuvers���Naval Postgraduate School, 699 Dyer Rd, Rm 137, Monterey, CA 93943-5000, Voice: 831-656-2074, Fax: 831-656-2313, [email protected]�Ross Pap.pdf�$Aerobraking~
�	,@�
���P`@M���@M���@Y�NPHerman, Albert L., PhD                                         Spencer, David B.=�N4Optimal, Low-Thrust, LEO to GEO/MEO/HEO Trajectories��N�(Herman) Spectrum Astro, Inc, 1440 North Fiesta Blvd., Gilbert, AZ 85233, Voice: 602-892-8200, Fax: 602-892-2949, [email protected] (Spencer) Air Force Research Laboratory/VSSS, Kirtland AFB, NM 87117-5776, [email protected] -�N$Abstract~from~Herman~and~Spencer.doc�OOptimization~
�	,@�
�USess 15�_Tethers - Arun Misra��```````a	�
TWed AM���2@;��@;��@E�<Biswell, Brian L.                          Puig-Suari, JordiN�EAltitude Control of a Tethered Lifting Probe for Atmospheric Research���(Biswell) Raytheon Systems Company, MS 805/M4, POB 11337, Tucson, AZ  85734-1337, [email protected], Voice: 520-794-8719 (Puig-Suari) Aeronautical Engineering Dept, California Polytechnic Univ, San Luis Obispo, CA  93407�!�JTether, Attitude Control~
�	.@�
���3@<��@<��@E�<Biswell, Brian L.                          Puig-Suari, JordiD�;Improved Tether Aerobraking Maneuvers Using a Lifting Probe���(Biswell) Raytheon Systems Company, MS 805/M4, POB 11337, Tucson, AZ  85734-1337, [email protected], Voice: 520-794-8719 (Puig-Suari) Aeronautical Engineering Dept, California Polytechnic Univ, San Luis Obispo, CA  93407��$Tether ~
�	.@�
����L@<��@<��@n�eGates, Stephen S.                          Koss, Stephen M.                          Zedd, Michael F.L�CLessons Learned About the Deployment Malfunction of the ATEx Tether���Naval Research Lab, Code 8233, 4555 Overlook Ave SW, Washington DC 20375-5355, Voice: 202-404-8337, Fax: 202-404-7785, [email protected]��$Tether~
�	.@�
����Z@< ��@<���@�Mazzoleni, Andre P.R�IA Study of the Deployment Dynamics of the ASTOR Tethered Satellite System���Dept of Eng, Texas Christian Univ, Box 298640, Fort Worth, TX 76129, Voice: 817-257-6317, Fax: 817-257-7704, [email protected] �Abstract for Alaska.doc�?Tether~
�	.@�
���@T@<���@<��@m�dCicci, David A, Dr.                   Lovell, T.A.                                        Qualls, C.X�OA Look at Tethered Satellite Identification Using Ridge-Type Estimation Methods���Aerospace Engineering Dept, 211 Aerospace Engineering Bldg, Auburn Univ, Auburn, AL 36849-5338, Voice: 334-844-6820, Fax: 334-844-6803, [email protected]�$�$Tether, Orbit Determination~
�	.@�
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�< ���Cochran, J.E. Jr.                                   Cho, S.                                    Lovell, A.                                     Cicci, D.A.R�IModeling Tethered Satellite Systems for Detection and Orbit Determinationn�eAuburn Univ, 211 Aerospace Engineering Bldg, Auburn, AL 36849, Voice: 334-844-4874, Fax: 334-844-6803�$�$Tether, Orbit Determination~
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���P@b@M���@M���@r�NiBarnds, Jim                                       Coffey, Shannon                             Davis, Mark0�N'Tracking of the TiPS Tethered Satellite#�N[email protected]�N�OTether~
�	.@�
�USess 16+�_"Prediction/Uncertainty - Beny Neta��```````a	�
TWed PM���=@;@��@;@��@C�:Chesley, Steve                              Milani, AndreaE�<Nonlinear Methods for the Propagation of Orbital Uncertainty���Dipartimento di Matematica, Via Buonarroti 2, 56127 Pisa, Italy, Voice: +39-050-844274, Fax: +39-050-844224, [email protected]��JPrediction Uncertainty~
�	0@�
����E@<���@�<N/AG�>Hoots, Felix R.                             France, Richard G./�&Satellite Drag Error Growth Estimation���GRC International, Inc, 985 Space Center Dr, #310, Colorado Springs, CO 80915, Voice: 719-596-5395, Fax: 719-596-6139, [email protected]��$Prediction Uncertainty~
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���U@<���@<��@{�rJesus, Antonio Delson Conceicao de; Souza, Marcelo Lopes Loiveira e; Prado, Antonio Fernando Bertachini de AlmeidaV�MMonte-Carlo Analysis of Nonimpulsive Orbital Transfers Under Thrust Errors, 1��(Jesus) Universidade Estadual de Feira de Santana-UEFS, Feira de Santana, BA, Brasil, Voice/Fax: 55-75-2248-85; [email protected] (Souze, Prado) Instituto Nacional de Pesquisas Espaciais-S.Jose dos Campos, SF, 12227-010, Voice: 55-12-3456201, Fax: 55-12-3456226�AAS1.doc�$Optimization~
�	0@�
���@W@<��@< ��@G�>Walker, Cheryl A.H.                         Casali, Stephen J.w�nImproved Space Surveillance Network Observation Error Modeling and Techniques for Force Model Error Mitigation���ITT Industries, 4450 E. Fountain Blvd, Colorado Springs, CO 80916 (Walker) Voice: 719-637-5938, Fax: 719-637-5960, [email protected] (Casali) Voice: 719-591-3663, Fax: 719-637-5960, [email protected] ^�Uextabs.doc                                       extabs.ppt (takes too long to print)�$Prediction Error~
�	0@�
����]@<���@<���@F�=Alfriend, Kyle T.                                Paik, Sokwon^�UCovariance as an Estimator of Orbit Prediction Error Growth for Geosynchronous Orbits��}Texas A&M Univ, H.R. Bright Bldg, Rm 701, College Station, TX, Voice: 409-845-5920, Fax: 409-845-6051, [email protected]�GEO Study Abstract.doc�$Prediction Error~
�	0@�
���^@<���@<���@M�DAlfriend, Kyle T.                                Wilkins, Matthew P.m�dCovariance as an Estimator of Orbit Prediction Error Growth in the Presence of Unknown Sensor Biases��}Texas A&M Univ, H.R. Bright Bldg, Rm 701, College Station, TX, Voice: 409-845-5920, Fax: 409-845-6051, [email protected]�Biases-Abstract.doc�$Prediction Error~
�	0@�
���P�_@M���@M���@�NMenon, Premkumar R.0�N'Stardust Navigation Covariance Analysis��N�Jet Propulsion Lab, 4800 Oak Grove Dr, California Institute of Technology, Pasadena,  CA 91109, Voice: 818-354-5093, [email protected]�NAIAA99 Abstract.doc�OAccuracy, Covariance~
�	0@�
����Z@< ��@<���@�Snow, Daniel3�*Element Set Prediction Accuracy Assessment)� [email protected]�
ABSTRACT1.doc�?Prediction Error~
�	0@�
�USess 17+�_"Attitude Estimation - Don Mackison��```````a	�
TWed PM���I@<���@<��@D�;Oshman, Y.                                       Dellus, F.`�WSpacecraft Angular Velocity Estimation Using Sequential Observations of a Single Vector��(Oshman) Dept of Aerospace Engineering, Technion - Israel Institute of Technology, Haifa 32000, Israel, Voice: +972-4-829-3803, Fax: +972-823-1848, [email protected] (Dellus) MBT Systems and Space Technology, Electronic Division, Israeli Aircraft I�asc99.pdf; asc99.ps�$Attitude Estimation~
�	1@�
���:@<@��@<@��@A�8Markley, F. Landis                      Mortari, Daniele:�1How to Estimate Attitude from Vector Observations���(Markley) NASA's Goddard Space Flight Center, Greenbelt, MD, [email protected] (Mortari) Univ of Rome "La Sapienza", Rome, ItalyX�OAbstract.doc                    CoverLetter.doc               fig1.ps & fig2.ps�$Attitude Estimation~
�	1@�
���*@<���@
�< x�oFengqi, Zhou                                    Hui, Liao,                                            Jun, ZhouV�MApplication of Extended Kalman Filter for Small Satellite Attitude Estimationz�qPOB 250, College of Astronautics, Northwestern Polytechnical Univ, Xi'an   710072, the People's Republic of China��$Attitude Estimation~
�	1@�
���"@< ��@< ��@�Schaechter, David<�3A Fully-Redundant Set of Single-Axis Accelerometers���Lockheed Martin Missiles & Space, Advanced Technology Center, 3251 Hanover Street, Bldg 250, Org H1-61, Palo Alto, CA  94304, [email protected]>�51999_Astro_Submittal.doc; 1999_Astrodynamics_Conf.doc�$Attitude Estimation~
�	1@�
���8@< ��@<@��@�Peck, Mason _�VMass-Properties Estimation for Spacecraft with powerful Fuel Damping Extended Abstract���Hughes Space & Communications, 2000 E. El Segundo Blvd, POB 902, El Segundo, CA 90245-4709, Voice: 310-416-5127, Fax: 310-416-5188, [email protected]��$Attitude Estimation~
�	1@�
���H@<���@<��@k�bJu, Gwanghyoek                                Pollack, Tom                        Junkins, John L.`�WDIGISTAR II Micro-Star Tracker: Autonomous On-Orbit Calibration and Attitude Estimation���Texas A&M Univ, College Station, TX, Voice: 409-845-0720 (Home) 2500 Central Park Ln #2105, College Station, TX 77840, [email protected]1�(Alaska99Abstract.doc; Alaska99Letter.doc�$Attitude Estimation~
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���P�I@M��@M��@�NRaman, Kidambi V.H�N?Multiple Approaches for GYRO Calibration of INTELSAT Satellites��N�INTELSAT, Box#60, 3400 International Dr NW, Washington DC 20008-3098, Voice: 202-944-7581, Fax: 202-944-7032, [email protected]�Ndcalabs.doc�OAttitude Estimation~
�	1@�
���@;��@;��@�Haley, David R.l�cPrecision Attitude Estimation with Star Trackers: Experience, Error Models an Their Interpretation ��zSpace Dept, Johns Hopkins Univ, APL, Laurel, MD 20723-6099, Voice: 240-228-5206, Fax: 240-228-1093, [email protected]�Abstract1_AK.doc�JAttitude Estimation~
�	1@�
����F@<���@<��@��Misra, Arun K.                       Sedlak, Joseph                                Gregory, Jim; Jones, Sonny                                      Smilek, Ron ; Lorentz, Dave                                         Bowser, Robert; Mylod, Pat              X�OLandsat-4 Attitude Recovery and Other Experiences with Aging Landsat Spacecraft���(Misra, Sedlak, Gregory, Jones, Smilek) Computer Sciences Corp, 4300 Forbes Blvd, Lanham, MD 20706, Voice: 301-552-0506, Fax: 301-552-3028, [email protected] (Lorentz) SGT, Inc., Greenbelt, MD (Bowser, Mylod) Space Imaging, Denver, CO��$Attitude Estimation~
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�D�6lL�V'b���x��,p��Qu��s�p6�����u��JT0@ ��b��b��b����������b��b��� �,%@ ���b��b������b�����������{�� � ���b��������b��{�����z0������� �;0@� ���S1�_(Guidance and Navigation - Bobby Williams��```````aK
���@; ��@;@��@H�?Ong, Kwok M., Dr.                               Kamel, Ahmed A.G�>Image Navigation Based on Landmark and Earth Edge Measurements��Space Systems/LORAL, MS G-76, 3825 Fabian Way, Palo Alto, CA  94303, Voice: 650-852-4909, Fax: 650-852-4666, [email protected]��J
Navigation~
�	2@�
����K@<��@< ��@H�?Fisher, Jeff Wesley                        Trochman, William R.J�ATheory and Flight Performance of the Magnetic Orbital Gyrocompass�[email protected]�AbstractSubmittal�$
Navigation~
�	2@�
���@R@< ��@<@��@���Folta, David                                 Gramling, Cheryl                          Leung, Dominic                               Belur, Sheela                                 Long, Anne6�-Autonomous Navigation Using Celestial Objects���(Folta/Gramling) NASA Goddard Space Flight Center, Code 571, Greenbelt, MD 20771, Voice: 301-286-6082, Fax: 301-286-1719, [email protected] (Leung/Belur/Long) Computer Sciences Corporation�
CelNav.doc�$
Navigation~
�	2@�
���T@<@��@<��@���Mase, Robert A.                         Spencer, David A.                       Smith, John C.                           Braun, Robert D., Dr.=�4Navigation Strategy for the Mars 2001 Lander Mission���(Mase, Spencer, Smith) Jet Propulsion Lab, California Institute of Technology, 4800 Oak Grove Dr, Pasadena, CA 91109-8099, Voice: 818-354-8990, Fax: 818-393-5261, [email protected] (Braun) NASA Langley Research Center �Abstract_Submission.pdf�$
Navigation~
�	2@�
����W@<��@�<Unsuccessful e-maily�pMortari, Daniele                              Barsocchi, Miro                              Castronuovo, Marco M.K�BEarth-Sun Attitude Sensor: Data Processing and Simulation Software��(Mortari/Castronuovo) Universita' degli Studi "La Sapienza" di Roma, Via Salaria, 851 - 00138 Roma, Italy, Voice: +39(06)812-0529, Fax: +39(06)810-5241, [email protected], [email protected] (Barsocchi) Via Cimabue, 7, 00034 �	miro1.bmp�$
Navigation~
�	2@�
���X@<��@�<Unsuccessful e-mailn�eMortari, Daniele                              Junkins, John                        Angelucci, MichelaU�LSP-Search Star Pattern Recognition ofr Multiple Fields of View Star Trackers��(Mortari/Angelucci) Universita' degli Studi "La Sapienza" di Roma, Via Salaria, 851 - 00138 Roma, Italy, Voice: +39(06)812-0529, Fax: +39(06)810-5241, [email protected] (Junkins) Texas A&M Univ, 722 Bright Blvd., College Station, TX 77843-3��$
Navigation~
�	2@�
���@X@<��@�<Unsuccessful e-mailE�<Mortari, Daniele                              Gigli, StefanoD�;Earth-Sun Attitude Sensor: Hardware Design and Ground Tests��(Mortari/Angelucci) Universita' degli Studi "La Sapienza" di Roma, Via Salaria, 851 - 00138 Roma, Italy, Voice: +39(06)812-0529, Fax: +39(06)810-5241, [email protected] (Gigli) Alenia Difesa, Divisione Sistemi Avionici ed Equipaggiamenti Un��$
Navigation~
�	2@�
����`@<���@<��@H�?Weeks, C.J.                                        Miller, J.K.���Calibration of Radiometric Data for General Relativity and Solar Plasma during the Near Earth Asteroid Rendezvous Spacecraft Solar Conjunction��(Weeks) Loyola Marymount Univ, 7900 Loyola Blvd, LAX, CA 90045-8130, Voice: 310-338-5108, Fax: 310-338-7339, [email protected] (Miller) Jet Propulsion Lab, California Institute of Technology, MS 301/125j, 4800 Oak Grove Dr, Pasadena,  CA 91109, Voice��$
Navigation~
�	2@�
���L`d@M���@M���@7�N.Ichikawa, Tsutomu                 Kato, Takaji,�N#Navigation of Mars Mission - NOZOMI��N�The Institute of Space and Astronautical Science, 3-1-1 Yoshinodai, Sagamihara, Kanagawa 229-8510, Japan, Voice/Fax: 81-42-759-8357, [email protected]�N�O
Navigation~
�	2@�
�S)�_ Orbit Dynamics - Paul Schumacher��```````aK
���M@;��@;��@�Miller, James G.4�+Velocity Distribution of Satellite Breakups�vThe MITRE Corp, 1150 Academy Park Loop, #212, Colorado Springs, CO 80910-3716, Voice: 719-572-8383, [email protected]��JBreakups~
�	3@�
����Q@<��@<@��@�Sonnabend, Dave�Toubles with Lambert~�uAnalytical Engineering, 5423 Glendale Gulch, Boulder, CO 80301-3537, Voice: 303-530-9641, [email protected]��$Lambert~
�	3@�
����R@<@��@<@��@G�>Kawaguchi, Jun                                Yoshikawa, ShojiT�KOn the Improved orbit Stability Criterion Around An Irregularly Shaped Body��(Kawaguchi) The Institute of Space and Astronautical Science, 3-1-1 Yoshinodai, Sagamihara, 229-8510, Japan, Voice: +81-42-759-8219, Fax: +81-42-759-8458, [email protected] (Yoshikawa) Advanced Technology R&D Center, Mitsubishi Electric Co., 8-1-1 �!�$Asteroids, Astrodynamics~
�	3@�
����_@<���@<���@�Seybold, Calina C.C�:Third Body Short-Period Terms in Analytic Orbit Predititon���The Univ of Texas at Austin, 3925 W. Braker Ln, #200, Austin, TX 78759-5321, Voice: 512-471-7175, Fax: 512-471-3585, [email protected]�abstractseybold.doc�$
Astrodynamics~
�	3@�
���@`@<���@<���@�Cangahuala, L.A.P�GThe Gravitational Potential of a Body in Terms of Ellipsoidal Harmonics���Jet Propulsion Lab, 4800 Oak Grove Dr, California Institute of Technology, MS 301-125J,  Pasadena, CA, Voice: 818-354-3606, [email protected])� Ellipsoidal.abstract.2.10.99.doc�$
Astrodynamics~
�	3@�
���@c@<��@<��@=�4Howell, K.C.                            Barden, B.T.�D�1Formation Flying Near the Sun-Earth/Moon L1 Point)+���Purdue Univ, 1282 Grissom Hall, West Lafayette, IN 47907-1282 (Howell) Voice: 765-494-5786, Fax: 765-494-0307, [email protected] (Barden) Voice: 765-494-5813, Fax: Same, [email protected]��$	Formation~
�	3@�
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�< a�XPourtakdoust, S.H.                        Mehri B.                    Novinzadch, A.R.B.~�uAn Investigation of Satellite Oscillations in an Arbitrary Orbit Using Regular Perturbation Theory and the WKB Methodf�]Sharif Univ of Technology, Dept of Mech Eng, Fax: 98-21-918-23-66, [email protected]?�
�$~
�	3@"�
QRejected by Session Chair��� e@<���@�<���Lo, Martin W.                       Koon, Wang Sang                           Ross, Shane                       Marsden, Jerrold                    7�.The Genesis Trajectory and Heteroclinic Cyclesf�]Jet Propulsion Lab, California Institute of Technology, 4800 Oak Grove Dr, Pasadena, CA 91109�
�$~
�	3@�
���L`e@M���@M���@�NWnuk, Edwine�N\Relation between Osculating and Mean Orbital Elements in the Case of the Second Order Theory��N�Astronomical Observatory of the A. Mickiewicz Univ, ul.Sloneczna 36, PL-60-286 Poznan, Poland, Voice/Fax: +48(61)8686511, [email protected]�N�O
Astrodynamics~
�	3@�
�S)�_ Attitude Dynamics - John Cochran��```````aK
���A@;`��@;@��@K�BJavorsek, Daniel II                        Longuski, James M.     O�FVelocity Pointing Errors Associated with Spinning Thrusting Spacecraft���Purdue Univ, 1282 Grissom Hall, West Lafayette, IN 47907-1282, Voice: 765-494-5139, Fax: 765-494-0307, Home Voice: 765-423-1287, [email protected]��JAttitude Control~
�	4@�
���B@<`��@<@��@q�hGick, R. Anne                               Williams, Marc H.                         Longuski, James M.d�[Periodic Solutions for a Spinning Asymmetric Rigid Body with Constant Principal-Axis Torque���Purdue Univ, 1282 Grissom Hall, West Lafayette, IN 47907-1282, Voice: 765-494-5139, Fax: 765-494-0307, Home Voice: 765-423-1287, [email protected]��$Attitude Theory~
�	4@�
����O@<��@< ��@#�Ying, Shuh-Jing (Benjamin)>�5Rotational Motions of a Satellite in a Circular Orbit��C�Dept of Mechanical Engineering, Univ of South Florida, 4202 East Fowler Avenue, ENB 118, Tampa, FL 33620-5350, Voice: 813-974-5627, Fax: 813-974-3539, [email protected]��$Attitude Estimation~
�	4@�
����R@<@��@<@��@���Misra, Arun K.                                              Min, B.                                                     Cyril, X.                                            Modi, V.J.                                                deSilva, C.W.O�FObject-Oriented Modeling of the Dynamics of Flexible Multibody Systems���McGill Univ, Dept of Mechanical Engineering, 817 Sherbrooke St. W, Montreal, QC, H3A 2K6, Voice: 514-398-6288, Fax: 514-398-7365, [email protected]��$Attitude-Flexible Body~
�	4@�
����U@<���@�<Unsuccessful e-mail�Ueno, Seiyac�ZTranslational Motion of Gravity Gradient Stabilized Satellites Due to Attitude Oscillation���Yokohama National Univ, 79-5 Tokiwadai Hodogaya-ku, Yokohama, 240-8501 Japan, Voice/Fax: +81-45-339-4242, [email protected]� �$Attitude, Astrodynamics~
�	4@�
���[@< ��@<���@H�?Eke, F.O.                                             Eke, E.M.X�OEffects of Internal Mass Flow on the Attitude Dynamics of Variable Mass Systems���(F.O.) Univ of California, One Shields Ave, Davis, CA 95616-5294, Voice: 530-752-2309, Fax: 530-752-4158, [email protected] (E.M.) 6000 J St, Sacramento, CA 95819-6031 �Aas=AIAAabstract-99.doc�?Attitude Theory~
�	4@�
����b@<���@<���@~�uMiller, Andrew J.                              Gray, Gary L.                                      Mazzoleni, Andre P.q�hNonlinear Dynamics of a Viscously Damped Spacecraft with a Flexible Appendage and Time-Dependent Forcing���The Pennsylvania State Univ, 227 Hammond Bldg, Univ Park, PA 16802-1401, Voice: 814-865-4523, Fax: 814-863-7967, [email protected]��$Attitude Control~
�	4@�
��� c@<��@<��@E�<Hall, Christopher D.                        Beck, Jeffrey A.2�)Relative Equilibria of Orbiting Gyrostats���(Hall) Virginia Polytechnic Institute & State Univ, Blacksburg, VA 24061, Voice: 540-231-2314, Fax: 540-231-9632, [email protected] (Beck) Air Force Research Lab, Kirtland AFB, NM 87117��$Attitude Theory~
�	4@�
���Le@M���@�M�NMitchell, Jason Wm.��NA Simplified Variation of Parameters Formulation of Euler's Equations of Motion of an Arbitrarily Torqued Asymmetric Rigid Body��N�Univ of Cincinnati, Dept of Aeospace Eng & Eng Mechanics, ML70, Cincinnati, OH 45221-0070, Voice: 513-556-6499 Fax: 513-556-5038, [email protected]�
�NO~
�	4@�
�S;�_2Asteroids and Comets - Victoria Coverstone-Carroll��```````aK
���@; ��@;@��@C�:Friedlander, Alan                            Niehoff, John7�.Rendezvous Mission to a First-Apparition Comet��zSAIC, 1501 Woodfield Road, #202 N, Schaumburg, IL  60173, Voice: 847-330-2518, Fax: 847-330-2522, [email protected]��JMission Design~
�	5@�
�DB5l[�.@D]PRrS5w����~S���i�����e��T0��b��b��b�`	��������b���V�����%���b��b������b� ��&@<`��@<`��@�Markopoulos, Nikosf�]How Much Thrust, Energy, or Propellant Does it take to Guide a Natural Celestial Body? (None)���School of Aerospace Engineering, Georgia Institute of Technology, 270 Ferst Drive, Atlanta, GA  30332-0150, Voice: 404-894-3066, Fax: 404-894-2760, [email protected]��$Asteroids??~
�	5@��>@<@��@<@��@C�:Chesley, Steve                              Milani, Andrea>�5Asteroid Close Encounters with Earth: Risk Assessment���Dipartimento di Matematica, Via Buonarroti 2, 56127 Pisa, Italy, Voice: +39-050-844274, Fax: +39-050-844224, [email protected]��$Prediction Uncertainty~
�	5@��K@<��@<��@G�>Chodas, Paul W.                             Yeomans, Donald K._�VPredicting Close Approaches and Estimating Impact Probabilities for Near-Earth Objects��(Chodas) Jet Propulsion Lab, California Institute of Technology, 4800 Oak Grove Dr, MS 301-150G, Pasadena, CA 91109-8099, Voice: 818-354-7795, Fax: 818-393-1159, [email protected] (Yeomans) Voice: 818-354-2127, Fax: 818-393-1159, donald.yeomans@jpl�	Ast99.doc�$Close Approach ~
�	5@��@Q@<��@
�< ���Miller, James K.                           Antreasian, P.J.                            Giorgini, J.                                    Owen, W.M.                                Williams, B.G.                              Yeomans, D.K.l�cDetermination of Eros Physical Parameters for Near Earth Asteroid Rendezvous Orbit Phase Navigation���Jet Propulsion Lab, California Institute of Technology, MS 301/125J, 4800 Oak Grove Dr, Pasadena, CA 91109-8099, Voice: 818-354-4321��$	Asteroids~
�	5@���V@<���@<��@��Antreasian, P.G.                              Helfrich, C.L.                                     Miller, J.K.; Owen, W.M.                                       Williams, B.G.                                   Yeomans, D.K.                                 L�CPreliminary Planning for NEAR's Low-Altitude Operations at 433 Eros��(Antreasian, Helfrich, Miller, Owen, Williams, Yeomans, Giorgini) Jet Propulsion Lab, California Institute of Technology, 4800 Oak Grove Dr, Pasadena, CA 91109-8099, Voice: 818-354-4381, Fax: 818-393-5214, [email protected] (Scheeres) Dept of Aerospace��$Asteroid~
�	5@���V@<��@<��@H�?Chern, Jeng-Shing                               Sheu, Dong-Long@�7Deviating an Earth-Pointing Asteroid under Lunar Effect���(Chern) Chung Shan Institute of Science and Technology, POB 90008-6-7, Lungtan, Taiwan 32526, R.O.C., [email protected] (Sheu) IAA, National Cheng Kung Univ, Tainan, Taiwan 70101, R.O.C.�	AAS01.doc�$Asteroid~
�	5@��Z@< ��@< ��@��Helfrich, C.E.                                     Miller, J.K.                                           Antreasian                           Carranza, E.                                       Williams, B.G.                                        Dunham,Y�PNear Earth Asteroid Rendezvous (Near) Revised EROS orbit Phase Trajectory Design��(Helfrich, Miller, Antreasian, Carranza, Williams) Jet Propulsion Lab, California Institute of Technology, M/S 301-150, 4800 Oak Grove Dr, Pasadena, CA 91109-8099, Voice: 818-354-1446, Fax: 818-393-6388, [email protected] (Dunham, Farquhar, McAd��$Asteroid~
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�M �NDesai, Prasun N. Q�NHEntry Dispersion Analysis for the Muses-C Asteroid Sample Return CapsuleF�N=NASA Langley Research Center, MS 365, Hampton, VA 23681-2199 �N�OMission Design~
�	5@��WXXYYYYZV	���e@<���@$�DThis is a duplicate of # 31l�cNicholas, A.C.                             Picone, J.M.                              Thonnard, S.E.{�rA Methodology for Using Optimal MSIS Parameters Retrieved from SSULI Data to Compute Satellite Drag on LEO ObjectsM�DNaval Research Lab, Washington, DC  20375, [email protected]�%�$Atmospheric Density (Marcos)�	���f@<`��@#�DThis is a duplicate of # 7>�5Pardini, C.                               Anselmo, L.z�qCalibration of Semi-Empirical Atmosphere Models through the Orbital Decay of Spherical and Cylindrical Satellites7�.[email protected]; [email protected]�%�$Atmospheric Density (Marcos)�	���f@<`��@$�DThis is a duplicate of # 47���Tolson, R.H.                               Keating, G.M.                          Baird, D.T.                           Noll, S.N.                             Shellenberg, T.I.X�OUtilization of Mars Global Surveyor Accelerometer Data for Atmospheric Modeling �[email protected]�%�$Atmospheric Density (Marcos)�	~
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