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<div class=Section1>
<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>CALL
FOR PAPERS<o:p></o:p></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>The
19<sup>th</sup> AAS/AIAA Space Flight Mechanics Meeting<o:p></o:p></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>Hilton
Savannah Desoto, Savannah, Georgia<o:p></o:p></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: October 6, 2008<o:p></o:p></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 19<sup>th</sup> Space Flight Mechanics Meeting will be
held February 8 - 12, 2009, at the Hilton Savannah Desoto in Savannah, Georgia.
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:<o:p></o:p></span></p>
<table border=0 cellspacing=0 cellpadding=0 style='border-collapse:collapse;
mso-table-layout-alt:fixed;mso-padding-alt:0in 5.4pt 0in 5.4pt'>
<tr style='height:167.65pt'>
<td width=239 valign=top style='width:239.4pt;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<o:p></o:p></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<o:p></o:p></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<o:p></o:p></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<o:p></o:p></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<o:p></o:p></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 <o:p></o:p></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<o:p></o:p></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<o:p></o:p></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<o:p></o:p></span></p>
</td>
<td width=239 valign=top style='width:239.4pt;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<o:p></o:p></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<o:p></o:p></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<o:p></o:p></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<o:p></o:p></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<o:p></o:p></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<o:p></o:p></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)<o:p></o:p></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<o:p></o:p></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.<o:p></o:p></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.<o:p></o:p></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<o:p></o:p></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.<o:p></o:p></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<o:p></o:p></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'>.<br clear=ALL style='page-break-before:always'>
</span><span style='font-size:11.0pt;color:windowtext'><b>INFORMATION FOR
AUTHORS<o:p></o:p></b></span></p>
<p class=default><span style='font-size:11.0pt'>The official conference website
is located at:<br>
<span style="mso-spacerun: yes"> </span></span><a
href="http://www.space-flight.org/AAS_meetings/2009_winter/2009%20winter.html">http://www.space-flight.org/AAS_meetings/2009_winter/2009
winter.html</a><span style='font-size:11.0pt'>, <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.<o:p></o:p></span></p>
<p class=default><span style='font-size:11.0pt'>The abstract submission
deadline is October 6, 2008. 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 November 17, 2008.<o:p></o:p></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:<o:p></o:p></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;mso-list:l0 level1 lfo1;
tab-stops:.25in'><![if !supportLists]><span style='font-size:11.0pt'>1.<span
style='font:7.0pt "Times New Roman"'> </span></span><![endif]><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.<o:p></o:p></span></p>
<p class=default style='margin-top:0in;margin-right:0in;margin-bottom:0in;
margin-left:.25in;margin-bottom:.0001pt;text-indent:-.25in;mso-list:l0 level1 lfo1;
tab-stops:.25in'><![if !supportLists]><span style='font-size:11.0pt'>2.<span
style='font:7.0pt "Times New Roman"'> </span></span><![endif]><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.<o:p></o:p></span></p>
<p class=default style='margin-top:0in;margin-right:0in;margin-bottom:14.0pt;
margin-left:.25in;text-indent:-.25in;mso-list:l0 level1 lfo1;tab-stops:.25in'><![if !supportLists]><span
style='font-size:11.0pt'>3.<span style='font:7.0pt "Times New Roman"'>
</span></span><![endif]><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.<o:p></o:p></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.<o:p></o:p></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.<o:p></o:p></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.<span style="mso-spacerun: yes">
</span>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.<o:p></o:p></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:<o:p></o:p></span></p>
<table border=0 cellspacing=0 cellpadding=0 style='border-collapse:collapse;
mso-table-layout-alt:fixed;mso-padding-alt:0in 5.4pt 0in 5.4pt'>
<tr>
<td width=239 valign=top style='width:239.4pt;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<o:p></o:p></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.
Alan M. Segerman<br>
AT&T Government Solutions, Inc.<br>
Naval Research Laboratory<br>
Code 8233<br>
4555 Overlook Ave., SW<br>
Washington, DC 20375-5355<br>
(202) 767-3819 / Fax (202) 404-7785<br>
</span><a href="mailto:[email protected]">[email protected]</a><span
style='font-size:10.0pt;color:windowtext'> <o:p></o:p></span></p>
</td>
<td width=239 valign=top style='width:239.4pt;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<o:p></o:p></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.
Peter C. Lai<br>
Aerospace Corporation<br>
Mail Stop: M4-895<br>
2350 E. El Segundo Blvd.<br>
El Segundo, CA 90245-4691<br>
(310) 336-2367<br>
</span><a href="mailto:[email protected]">[email protected]</a><span
style='font-size:11.0pt;color:windowtext'><o:p></o:p></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:<o:p></o:p></span></p>
<table border=0 cellspacing=0 cellpadding=0 style='border-collapse:collapse;
mso-table-layout-alt:fixed;mso-padding-alt:0in 5.4pt 0in 5.4pt'>
<tr>
<td width=239 valign=top style='width:239.4pt;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<o:p></o:p></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.
Matthew P. Wilkins<br>
Schafer Corporation<br>
AFRL/DESM<br>
550 Lipoa Parkway<br>
Kihei, HI 96753<br>
(808) 891-7747 / Fax (808) 874-1603<br>
</span><a href="mailto:[email protected]">[email protected]</a><span
style='font-size:10.0pt;color:windowtext'><b><o:p></o:p></b></span></p>
</td>
<td width=239 valign=top style='width:239.4pt;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<o:p></o:p></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.
Mark E. Pittelkau<br>
Aerospace Control Systems<br>
Engineering and Research, LLC<br>
35215 Greyfriar Drive<br>
Round Hill, VA 20141-2395<br>
(540) 751-1110 / Fax (540) 751-1116<br>
</span><a href="mailto:[email protected]">[email protected]</a><o:p></o:p></p>
</td>
</tr>
</table>
<p class=WW-Default style='margin-top:6.0pt;margin-right:0in;margin-bottom:
3.0pt;margin-left:0in'><![if !supportEmptyParas]> <![endif]><o:p></o:p></p>
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