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<row><id>1002</id><tag>congress</tag><pathname>IAC-10</pathname><relpath>../../</relpath><name>IAC-10</name><caption>61st International Astronautical Congress</caption></row>
<row><id>1224</id><tag>symposium</tag><pathname>IAC-10/C1</pathname><relpath>../</relpath><name>C1</name><caption>ASTRODYNAMICS SYMPOSIUM</caption></row>
<row><id>1227</id><tag>session</tag><pathname>IAC-10/C1/5</pathname><relpath/><name>5</name><caption>Guidance, Navigation, and Control</caption></row>
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<row><id>1227</id><tag>session</tag><pathname>IAC-10/C1/5</pathname><name>5</name><title xsi:nil="true"/><caption>Guidance, Navigation, and Control</caption><descr>The emphasis of this theme is on the studies and application related to the guidance, navigation and control of earth-orbiting and interplanetary spacecraft and rockets, including rendezvous and docking.</descr><Date>2010-09-29 15:15</Date><Room>North Hall</Room></row>
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<resultset>
<row><hello>Dr.</hello><first>Brij</first><last>Agrawal</last><email>agrawal@nps.edu</email><company>Naval Postgraduate School</company><country>United States</country><func>ipc.chairman</func><function>Chair</function></row>
<row><hello>Dr.</hello><first>Alfred</first><last>Ng</last><email>alfred.ng@asc-csa.gc.ca</email><company>Canadian Space Agency</company><country>Canada</country><func>ipc.chairman</func><function>Chair</function></row>
<row><hello>Dr.</hello><first>Fuyuto</first><last>Terui</last><email>terui.fuyuto@jaxa.jp</email><company>Japan Aerospace Exploration Agency (JAXA)</company><country>Japan</country><func>ipc.rapporteur</func><function>Rapporteur</function></row>
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<row><id>6565</id><sequence>1</sequence><revise>withdrawn</revise><Mode/><title>On the Calculus of Variations in the Optimal Spacecraft Formation Flying Path Planning</title><username>andrea.lafflitto</username><author>Mr. Andrea L'Afflitto</author><company>Virginia Tech</company><country>United States</country></row>
<row><id>7517</id><sequence>2</sequence><revise>confirmed</revise><Mode/><title>Attitude Manoeuvring Under Dynamic  Path  and  Time Constraints  for Improved GPS Coverage of Formation-Flying Nanosatellites</title><username>bryanjl</username><author>Mr. Bryan Johnston-Lemke</author><company>Space Flight Laboratory, University of Toronto</company><country>Canada</country></row>
<row><id>8736</id><sequence>3</sequence><revise>confirmed</revise><Mode/><title>Image based navigation and guidance for approach and touchdown phase to an asteroid utilizing captured images at the rehearsal operation</title><username>terui</username><author>Dr. Fuyuto Terui</author><company>Japan Aerospace Exploration Agency (JAXA)</company><country>Japan</country></row>
<row><id>8106</id><sequence>4</sequence><revise>confirmed</revise><Mode/><title>Formation acquisition and control strategies for formations in highly elliptic orbits</title><username>tpeters</username><author>Mr. Thomas Vincent Peters</author><company>GMV Aerospace &amp; Defence SAU</company><country>Spain</country></row>
<row><id>6944</id><sequence>5</sequence><revise>confirmed</revise><Mode/><title>Guidance and Control Strategies for a Spacecraft to Rendezvous with a Non-cooperative Spacecraft</title><username>komanduri</username><author>Mr. Ananth S. Komanduri</author><company>ZARM - University of Bremen</company><country>Germany</country></row>
<row><id>7115</id><sequence>6</sequence><revise>confirmed</revise><Mode/><title>Development of Sliding Mode Controller for Small Satellite in Planetary Orbital Environment Formation Flying Missions</title><username>saptarshi.bandyopadhyay@gmail.com</username><author>Mr. Saptarshi Bandyopadhyay</author><company>Indian Institute of Technology</company><country>India</country></row>
<row><id>6253</id><sequence>7</sequence><revise>confirmed</revise><Mode/><title>A new method of navigation and guidance using double line-of-sight measurements for autonomous rendezvous</title><username>AstroChet</username><author>Dr. Chen Tong</author><company>BUAA</company><country>China</country></row>
<row><id>7724</id><sequence>8</sequence><revise>confirmed</revise><Mode/><title>Approach for Optimal Multi-Rendezvous Trajectory Design for Active Debris Removal</title><username>junkokekokko</username><author>Ms. junko murakami</author><company>Kyushu University</company><country>Japan</country></row>
<row><id>7376</id><sequence>9</sequence><revise>confirmed</revise><Mode/><title>formation flight line of sight guidance</title><username>aerglmn@aerodyne.technion.ac.il</username><author>Prof. Mauricio Moshe Guelman</author><company>Asher Space Research Institute, Technion, I.I.T.</company><country>Israel</country></row>
<row><id>8182</id><sequence>10</sequence><revise>withdrawn</revise><Mode/><title>CNES formation flying experiment on PRISMA: spacecraft reconfiguration and rendezvous within FFIORD mission</title><username>bergesjc</username><author>Mr. Jean-Claude Berges</author><company>Centre National d'Etudes Spatiales (CNES)</company><country>France</country></row>
<row><id>8180</id><sequence>11</sequence><revise>confirmed</revise><Mode/><title>Flight Results from SSC’s GNC Experiments within the PRISMA Formation Flying Mission</title><username>robin.larsson@ssc.se</username><author>Mr. Robin Larsson</author><company>OHB Sweden</company><country>Sweden</country></row>
<row><id>8016</id><sequence>12</sequence><revise>confirmed</revise><Mode/><title>FLIGHT RESULTS FROM THE AUTONOMOUS NAVIGATION AND CONTROL OF FORMATION FLYING SPACECRAFT ON THE PRISMA MISSION</title><username>deflorio</username><author>Mr. Sergio De Florio</author><company>University of Glasgow, Space Advanced Research Team</company><country>Germany</country></row>
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