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<div class=Section1>
<p class=WW-Default align=center style='margin-top:6.0pt;margin-right:-.25in;
margin-bottom:3.0pt;margin-left:-.25in;text-align:center'><span
style='position:absolute;z-index:0;left:0px;margin-left:0px;margin-top:1px;
width:102px;height:50px'><img width=102 height=50
src="a2009%20call%20for%20papers_files/image001.jpg"></span><span
style='color:windowtext'><b>CALL FOR PAPERS</b></span><span style='position:
absolute;z-index:1;left:0px;margin-left:679px;margin-top:0px;width:121px;
height:51px'><img width=121 height=51
src="a2009%20call%20for%20papers_files/image002.jpg"></span></p>
<p class=WW-Default align=center style='margin-top:6.0pt;margin-right:0in;
margin-bottom:3.0pt;margin-left:0in;text-align:center'><span style='color:windowtext'><b>The
2009 AAS/AIAA Astrodynamics Specialist Conference</b></span></p>
<p class=WW-Default align=center style='margin-top:6.0pt;margin-right:0in;
margin-bottom:3.0pt;margin-left:0in;text-align:center'><span style='color:windowtext'><b>Renaissance
Hotel, Pittsburgh, Pennsylvania</b></span></p>
<p class=WW-Default align=center style='margin-top:9.0pt;margin-right:0in;
margin-bottom:12.0pt;margin-left:0in;text-align:center'><span style='color:
windowtext'><b><u>ABSTRACT DEADLINE: April 1, 2009</u></b></span></p>
<p class=WW-Default style='margin-top:6.0pt;margin-right:0in;margin-bottom:
3.0pt;margin-left:0in;text-align:justify'><span style='font-size:11.0pt;
color:windowtext'>The 2009 Astrodynamics Specialist Conference will be held
August 9 - 13, 2009, at the Renaissance Hotel in Pittsburgh, Pennsylvania. The
conference is organized by the American Astronautical Society (AAS) Space
Flight Mechanics Committee and co-sponsored by the American Institute of
Aeronautics and Astronautics (AIAA) Astrodynamics Technical Committee. Papers are
solicited on topics related to space flight mechanics and astrodynamics,
including, but not limited to:</span></p>
<table border=0 cellspacing=0 cellpadding=0 style='border-collapse:collapse'>
<tr style='height:167.65pt'>
<td width=273 valign=top style='width:273.15pt;padding:0in 5.4pt 0in 5.4pt;
height:167.65pt'>
<p class=WW-Default style='margin-top:6.0pt;margin-right:0in;margin-bottom:
3.0pt;margin-left:6.75pt;text-indent:-6.75pt;layout-grid-mode:char'><span
style='font-size:10.0pt;color:windowtext'>� Asteroid and non-Earth orbiting
missions</span></p>
<p class=WW-Default style='margin-top:6.0pt;margin-right:0in;margin-bottom:
3.0pt;margin-left:5.85pt;text-indent:-5.85pt'><span style='font-size:10.0pt;
color:windowtext'>� Atmospheric re-entry guidance and control</span></p>
<p class=WW-Default style='margin-top:6.0pt;margin-right:0in;margin-bottom:
3.0pt;margin-left:6.75pt;text-indent:-6.75pt'><span style='font-size:10.0pt;
color:windowtext'>� Attitude dynamics, determination and control</span></p>
<p class=WW-Default style='margin-top:6.0pt;margin-right:0in;margin-bottom:
3.0pt;margin-left:6.75pt;text-indent:-6.75pt'><span style='font-size:10.0pt;
color:windowtext'>� </span><span style='font-size:10.0pt'>Attitude-sensor and
payload-sensor calibration</span></p>
<p class=WW-Default style='margin-top:6.0pt;margin-right:0in;margin-bottom:
3.0pt;margin-left:6.75pt;text-indent:-6.75pt'><span style='font-size:10.0pt;
color:windowtext'>� </span><span style='font-size:10.0pt'>Conjunction
assessment</span></p>
<p class=WW-Default style='margin-top:6.0pt;margin-right:0in;margin-bottom:
3.0pt;margin-left:5.85pt;text-indent:-5.85pt'><span style='font-size:10.0pt;
color:windowtext'>� Dynamical systems theory applied to space flight problems</span></p>
<p class=WW-Default style='margin-top:6.0pt;margin-right:0in;margin-bottom:
3.0pt;margin-left:6.75pt;text-indent:-6.75pt'><span style='font-size:10.0pt;
color:windowtext'>� Dynamics and control of large space structures and
tethers </span></p>
<p class=WW-Default style='margin-top:6.0pt;margin-right:0in;margin-bottom:
3.0pt;margin-left:5.85pt;text-indent:-5.85pt'><span style='font-size:10.0pt;
color:windowtext'>� Earth orbital and planetary mission studies</span></p>
<p class=WW-Default style='margin-top:6.0pt;margin-right:0in;margin-bottom:
3.0pt;margin-left:5.85pt;text-indent:-5.85pt'><span style='font-size:10.0pt;
color:windowtext'>� Flight dynamics operations and spacecraft autonomy</span></p>
<p class=WW-Default style='margin-top:6.0pt;margin-right:0in;margin-bottom:
3.0pt;margin-left:5.85pt;text-indent:-5.85pt'><span style='font-size:10.0pt;
color:windowtext'>� </span><span style='font-size:10.0pt'>History of the US
space program</span></p>
</td>
<td width=273 valign=top style='width:273.15pt;padding:0in 5.4pt 0in 5.4pt;
height:167.65pt'>
<p class=WW-Default style='margin-top:6.0pt;margin-right:0in;margin-bottom:
3.0pt;margin-left:6.75pt;text-indent:-6.75pt;layout-grid-mode:char'><span
style='font-size:10.0pt;color:windowtext'>� Orbit determination and
space-surveillance tracking</span></p>
<p class=WW-Default style='margin-top:6.0pt;margin-right:0in;margin-bottom:
3.0pt;margin-left:6.75pt;text-indent:-6.75pt'><span style='font-size:10.0pt;
color:windowtext'>� Orbital debris and space environment</span></p>
<p class=WW-Default style='margin-top:6.0pt;margin-right:0in;margin-bottom:
3.0pt;margin-left:5.85pt;text-indent:-5.85pt'><span style='font-size:10.0pt;
color:windowtext'>� Orbital dynamics, perturbations, and stability</span></p>
<p class=WW-Default style='margin-top:6.0pt;margin-right:0in;margin-bottom:
3.0pt;margin-left:6.75pt;text-indent:-6.75pt'><span style='font-size:10.0pt;
color:windowtext'>� </span><span style='font-size:10.0pt'>Rendezvous,
relative motion, proximity missions, and </span><span style='font-size:10.0pt;
color:windowtext'>formation flying</span></p>
<p class=WW-Default style='margin-top:6.0pt;margin-right:0in;margin-bottom:
3.0pt;margin-left:5.85pt;text-indent:-5.85pt'><span style='font-size:10.0pt;
color:windowtext'>� </span><span style='font-size:10.0pt'>Reusable launch
vehicle design, dynamics, guidance, and control</span></p>
<p class=WW-Default style='margin-top:6.0pt;margin-right:0in;margin-bottom:
3.0pt;margin-left:6.75pt;text-indent:-6.75pt'><span style='font-size:10.0pt;
color:windowtext'>� Satellite constellations</span></p>
<p class=WW-Default style='margin-top:6.0pt;margin-right:0in;margin-bottom:
3.0pt;margin-left:5.85pt;text-indent:-5.85pt'><span style='font-size:10.0pt;
color:windowtext'>� Spacecraft guidance, navigation and control (GNC)</span></p>
<p class=WW-Default style='margin-top:6.0pt;margin-right:0in;margin-bottom:
3.0pt;margin-left:5.85pt;text-indent:-5.85pt'><span style='font-size:10.0pt;
color:windowtext'>� Tethered Satellites</span></p>
<p class=WW-Default style='margin-top:6.0pt;margin-right:0in;margin-bottom:
3.0pt;margin-left:5.85pt;text-indent:-5.85pt'><span style='font-size:10.0pt;
color:windowtext'>� Trajectory / mission / maneuver design and optimization</span></p>
</td>
</tr>
</table>
<p class=WW-Default style='margin-top:6.0pt;margin-right:0in;margin-bottom:
3.0pt;margin-left:0in;text-align:justify'><span style='font-size:11.0pt'>Papers
will be accepted based on the quality of an extended abstract (see below), the
originality of the work and ideas, and the anticipated interest in the proposed
subject. Papers that contain experimental results or current data, or </span><span
style='font-size:11.0pt;color:windowtext'>report on ongoing missions,</span><span
style='font-size:11.0pt'> are especially encouraged.</span></p>
<p class=WW-Default style='margin-top:6.0pt;margin-right:0in;margin-bottom:
3.0pt;margin-left:0in;text-align:justify'><span style='font-size:11.0pt'>Final
manuscripts are required before the conference. The working language for the
conference is English.</span></p>
<p class=WW-Default style='margin-top:6.0pt;margin-right:0in;margin-bottom:
3.0pt;margin-left:0in;text-align:justify'><span style='font-size:11.0pt;
color:windowtext'><b>SPECIAL SESSIONS</b></span></p>
<p class=WW-Default style='margin-top:6.0pt;margin-right:0in;margin-bottom:
3.0pt;margin-left:0in;text-align:justify'><span style='font-size:11.0pt;
color:windowtext'>Proposals are being accepted for suitable special sessions,
including panel discussions, invited sessions, workshops, mini-symposia, and
technology demonstrations. A proposal for a topical panel discussion should
include the session title, a brief description of the discussion topic(s), and
a list of the speakers and their qualifications. For an invited session, workshop,
mini-symposium, or demonstration, a proposal should include the session title,
a brief description, and a list of proposed activities and invited speakers and
paper titles. Prospective session organizers should submit their proposals to
the Technical Chairs.</span></p>
<p class=WW-Default style='margin-top:6.0pt;margin-right:0in;margin-bottom:
3.0pt;margin-left:0in;text-align:justify'><span style='font-size:11.0pt;
color:windowtext'><b>BREAKWELL STUDENT TRAVEL AWARD</b></span></p>
<p class=WW-Default style='margin-top:6.0pt;margin-right:0in;margin-bottom:
3.0pt;margin-left:0in;text-align:justify'><span style='font-size:11.0pt;
color:windowtext'>The AAS Space Flight Mechanics Technical Committee announces
the John V. Breakwell Student Travel Award. This award provides travel expenses
for up to three (3) U.S. and Canadian students presenting papers at this conference.
Students wishing to apply for this award are strongly advised to submit their
completed paper by the abstract submittal deadline. The maximum coverage per
student is limited to $1000. Details and applications may be obtained via </span><a
href="http://www.space-flight.org/">http://www.space-flight.org/</a><span
style='font-size:11.0pt'>.</span></p>
<p class=WW-Default style='margin-top:12.0pt;margin-right:0in;margin-bottom:
3.0pt;margin-left:0in;text-align:justify'><span style='font-size:11.0pt;
color:windowtext'><b>INFORMATION FOR AUTHORS</b></span></p>
<p class=default><span style='font-size:11.0pt'>The official conference website
is located at:<br>
<a
href="http://www.space-flight.org/AAS_meetings/2009_astro/2009%20astro.html">http://www.space-flight.org/AAS_meetings/2009_astro/2009%20astro.html</a>,<br>
which is accessible from the AAS website at </span><a
href="http://www.space-flight.org/">http://www.space-flight.org/</a><span
style='font-size:11.0pt'>. Conference information, rules and regulations are
maintained and updated via the web; authors should refer to the official
website for the most current information.</span></p>
<p class=default><span style='font-size:11.0pt'>The abstract submission
deadline is April 1, 2009. Please be aware that this date has been set at the
latest possible date for the convenience of contributors and that <em>there are
no plans to defer this deadline</em> due to the constraints of the conference
planning schedule. Should the number of submissions exceed the limited number
of presentation slots, <em>preference will be given to the earliest submissions</em>.
Notification of acceptance will be sent via email by May 18, 2009.</span></p>
<p class=default><span style='font-size:11.0pt'>To submit an abstract, use the
web-based submission system accessible from the official conference website. By
submitting an abstract, the author affirms that the paper�s majority content
has not been previously presented or published elsewhere. Detailed author
instructions will be sent by email after the abstract has been submitted. As
part of the online submission process, authors are expected to provide:</span></p>
<p class=default style='margin-top:14.0pt;margin-right:0in;margin-bottom:0in;
margin-left:.25in;margin-bottom:.0001pt;text-indent:-.25in;tab-stops:.25in'><span
style='font-size:11.0pt'>1.</span><span style='font-size:7.0pt'>
</span><span style='font-size:11.0pt'>A paper title, as well as the name,
affiliation, postal address, telephone number, and email address of the
corresponding author.</span></p>
<p class=default style='margin-top:0in;margin-right:0in;margin-bottom:0in;
margin-left:.25in;margin-bottom:.0001pt;text-indent:-.25in;tab-stops:.25in'><span
style='font-size:11.0pt'>2.</span><span style='font-size:7.0pt'>
</span><span style='font-size:11.0pt'>A two page extended abstract of at least
500 words, in the Portable Document File (PDF) format. The extended abstract
should provide a clear and concise statement of the problem to be addressed, an
explanation of its significance, the proposed method of solution, the results
expected or obtained, and supporting tables and figures as appropriate. A list
of pertinent references should be included.</span></p>
<p class=default style='margin-top:0in;margin-right:0in;margin-bottom:14.0pt;
margin-left:.25in;text-indent:-.25in;tab-stops:.25in'><span style='font-size:
11.0pt'>3.</span><span style='font-size:7.0pt'>
</span><span style='font-size:11.0pt'>A condensed abstract (100 words maximum)
to be included in the printed conference program. The condensed abstract is to
be entered into the text box provided on the web page, and must avoid the use
of special symbols or characters, such as Greek letters.</span></p>
<p class=WW-Default style='margin-top:6.0pt;margin-right:0in;margin-bottom:
3.0pt;margin-left:0in;text-align:justify'><span style='font-size:11.0pt;
color:windowtext'><b>Technology Transfer Warning - </b></span><span
style='font-size:11.0pt;color:windowtext'>Technology transfer guidelines
substantially extend the time required to review abstracts and papers by
private enterprises and government agencies. These reviews can require four
months or more. To preclude late submissions and paper withdrawals, it is the
responsibility of the author(s) to determine the extent of necessary approvals
prior to submitting an abstract.</span></p>
<p class=WW-Default style='margin-top:6.0pt;margin-right:0in;margin-bottom:
3.0pt;margin-left:0in;text-align:justify'><span style='font-size:11.0pt;
color:windowtext'><b>Visas – </b></span><span style='font-size:11.0pt;
color:windowtext'>Applications for visas to enter the Unites States can take
more than six months in some cases. Be sure to apply for a visa well in advance
of the conference.</span></p>
<p class=WW-Default style='margin-top:6.0pt;margin-right:0in;margin-bottom:
3.0pt;margin-left:0in;text-align:justify'><span style='font-size:11.0pt;
color:windowtext'><b>No Paper / No Podium and No Podium / No Publication Policy
- </b></span><span style='font-size:11.0pt;color:windowtext'>Completed
manuscripts are to be electronically uploaded to the web site prior to the
conference in PDF format,</span><span style='font-size:11.0pt'> be no more than
twenty pages in length, and</span><span style='font-size:11.0pt;color:windowtext'>
</span><span style='font-size:11.0pt'>conform to the AAS paper format</span><span
style='font-size:11.0pt;color:windowtext'>. If the completed manuscript is not
contributed on time, then it will not be presented at the conference and will
not appear in the conference proceedings. Any paper which is not presented for
any reason will be considered to be withdrawn and will not appear in the
conference proceedings. Prior to presentation, the presenting author will
provide the session chair with a short biographical sketch and, if requested, a
paper copy of the manuscript and presentation.</span></p>
<p class=WW-Default style='margin-top:6.0pt;margin-right:0in;margin-bottom:
3.0pt;margin-left:0in;text-align:justify'><span style='font-size:11.0pt;
color:windowtext'>Questions concerning the submission of papers should be
addressed to the technical chairs:</span></p>
<table border=0 cellspacing=0 cellpadding=0 style='border-collapse:collapse'>
<tr>
<td width=275 valign=top style='width:274.95pt;padding:0in 5.4pt 0in 5.4pt'>
<p class=WW-Default style='margin-top:6.0pt;margin-right:0in;margin-bottom:
3.0pt;margin-left:0in;layout-grid-mode:char'><span style='font-size:10.0pt;
color:windowtext'><b>AAS Technical Chair</b></span></p>
<p class=WW-Default style='margin-top:6.0pt;margin-right:0in;margin-bottom:
3.0pt;margin-left:0in'><span style='font-size:10.0pt;color:windowtext'>Dr.
Anil V. Rao<br>
Assistant Professor<br>
Dept. of Mechanical and Aerospace Engineering<br>
University of Florida, 314 MAE-A<br>
P.O. Box 116250<br>
Gainesville, FL 32611-6250<br>
(352) 392-5523<br>
[email protected]</span></p>
</td>
<td width=275 valign=top style='width:274.95pt;padding:0in 5.4pt 0in 5.4pt'>
<p class=WW-Default style='margin-top:6.0pt;margin-right:0in;margin-bottom:
3.0pt;margin-left:0in;layout-grid-mode:char'><span style='font-size:10.0pt;
color:windowtext'><b>AIAA Technical Chair</b></span></p>
<p class=WW-Default style='margin-top:6.0pt;margin-right:0in;margin-bottom:
3.0pt;margin-left:0in'><span style='font-size:10.0pt;color:windowtext'>Dr. T.
Alan Lovell<br>
AFRL/VSES<br>
Bldg. 593, Rm 10<br>
Kirtland AFB, NM 87117<br>
(505) 853-4132 (voice)<br>
[email protected]</span></p>
</td>
</tr>
</table>
<p class=WW-Default style='margin-top:6.0pt;margin-right:0in;margin-bottom:
3.0pt;margin-left:0in'><span style='font-size:11.0pt;color:windowtext'>All
other questions should be directed to the General Chairs:</span></p>
<table border=0 cellspacing=0 cellpadding=0 style='border-collapse:collapse'>
<tr>
<td width=275 valign=top style='width:274.95pt;padding:0in 5.4pt 0in 5.4pt'>
<p class=WW-Default style='margin-top:6.0pt;margin-right:0in;margin-bottom:
3.0pt;margin-left:0in;layout-grid-mode:char'><span style='font-size:10.0pt;
color:windowtext'><b>AAS General Chair</b></span></p>
<p class=WW-Default style='margin-top:6.0pt;margin-right:0in;margin-bottom:
3.0pt;margin-left:0in'><span style='font-size:10.0pt;color:windowtext'>Dr.
Ken Chan<br>
The Aerospace Corporation<br>
15049 Conference Center Drive<br>
Chantilly, VA 20151<br>
(571) 307-4211; (571) 307-4317 (Fax)<br>
[email protected]</span></p>
</td>
<td width=275 valign=top style='width:274.95pt;padding:0in 5.4pt 0in 5.4pt'>
<p class=WW-Default style='margin-top:6.0pt;margin-right:0in;margin-bottom:
3.0pt;margin-left:0in;layout-grid-mode:char'><span style='font-size:10.0pt;
color:windowtext'><b>AIAA General Chair</b></span></p>
<p class=WW-Default style='margin-top:6.0pt;margin-right:0in;margin-bottom:
3.0pt;margin-left:0in'><span style='font-size:10.0pt;color:windowtext'>Dr. L.
Alberto Cangahuala<br>
Deputy Manager, GN&C Section<br>
Jet Propulsion Laboratory<br>
MS 198-326<br>
4800 Oak Grove Drive<br>
Pasadena, CA 91109-8099<br>
818-354-3606 (voice); 818-393-4440 (Fax)<br>
[email protected]</span></p>
</td>
</tr>
</table>
<p class=WW-Default style='margin-top:6.0pt;margin-right:0in;margin-bottom:
3.0pt;margin-left:0in'> </p>
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