<caption>Orbital Dynamics - Part 1</caption><descr>This theme discusses advances in orbital dynamics, orbit determination, and orbit control. It includes orbital dynamics associated with constellations and formation flying.</descr><Date>2011-10-04 15:00</Date><Room>TS-04</Room></row> </resultset> <resultset> <row><hello>Prof.</hello><first>Rock Jeng-Shing</first><last>Chern</last><company>University of Science & Technology</company><country>Taiwan, China</country><func>ipc.chairman</func><function>Chairman</function></row> <row><hello>Prof.</hello><first>Filippo</first><last>Graziani</last><company>University of Rome “La Sapienza”</company><country>Italy</country><func>ipc.chairman</func><function>Chairman</function></row> <row><hello>Prof.</hello><first>Josep J.</first><last>Masdemont</last><company>Universitat Politecnica de Catalunya (UPC)</company><country>Spain</country><func>ipc.rapporteur</func><function>Rapporteur</function></row> </resultset> <resultset> <row><id>9272</id><sequence>1</sequence><revise>confirmed</revise><Mode/><title>Effect of a drag force due to absorption of solar radiation on solar sail orbital dynamics

1454congressIAC-11../../IAC-1162nd International Astronautical Congress 1467symposiumIAC-11/C1../C1ASTRODYNAMICS SYMPOSIUM 1529sessionIAC-11/C1/33Orbital Dynamics - Part 1 1529sessionIAC-11/C1/33<caption>Orbital Dynamics - Part 1</caption><descr>This theme discusses advances in orbital dynamics, orbit determination, and orbit control. It includes orbital dynamics associated with constellations and formation flying.</descr><Date>2011-10-04 15:00</Date><Room>TS-04</Room></row> </resultset> <resultset> <row><hello>Prof.</hello><first>Rock Jeng-Shing</first><last>Chern</last><company>University of Science & Technology</company><country>Taiwan, China</country><func>ipc.chairman</func><function>Chairman</function></row> <row><hello>Prof.</hello><first>Filippo</first><last>Graziani</last><company>University of Rome “La Sapienza”</company><country>Italy</country><func>ipc.chairman</func><function>Chairman</function></row> <row><hello>Prof.</hello><first>Josep J.</first><last>Masdemont</last><company>Universitat Politecnica de Catalunya (UPC)</company><country>Spain</country><func>ipc.rapporteur</func><function>Rapporteur</function></row> </resultset> <resultset> <row><id>9272</id><sequence>1</sequence><revise>confirmed</revise><Mode/><title>Effect of a drag force due to absorption of solar radiation on solar sail orbital dynamicsrkezerashviliProf. Roman Ya. KezerashviliNew York City College of TechnologyUnited States 96722confirmedAnalytical Solutions of the Relative Motion About a Keplerian Elliptic Orbitgerard.gomezProf. Gerard GomezUniversity of BarcelonaSpain 97833confirmedPost-aerocapture orbit selection and maintenance for the Aerofast mission to Marsmauro.pontani@tin.itDr. Mauro PontaniUniversity of Rome “La Sapienza”Italy 98994confirmedAn Extended Discussion on the DoubleStar OrbitsjstangDr. Jingshi TangNanjing UniversityChina 101325confirmedStation keeping of a solar sail in the solar systemariminusDr. Ariadna FarrésUniversité de BourgogneFrance 103406withdrawnIndia's first MARS Mission Orbit Determination Systemvignes@isac.gov.inDr. Narayanasetti Venkata VighnesamIndian Space Research Organization (ISRO)India 105457confirmedOptimal Impulsive Orbital Maneuver between Noncoplanar Noncoaxial orbits with or without Time constraintcivilProf. M. NavabiShahid Beheshti UniversityIran 107808confirmedNatural Periodic Relative Orbit Solving using Fourier Seriescaojing_495Ms. Jing CaoCollege of Astronautics,Northwestern Polytechnical UniversityChina 109409confirmedLong-term evolution of Galileo operational orbits by canonical perturbation theorymlara@roa.esDr. Martin LaraSpain 1168910confirmedSimulation of Orbit and Guidance Design for TSLVjschern@cc.hc.cust.edu.twProf. Rock Jeng-Shing ChernUniversity of Science & TechnologyTaiwan, China 1178711confirmedStability analysis of a highly eccentric orbit around Marsbpdaksha13Mrs. Bannihatti Parameshwarappa DakshayaniISRO Satellite Centre (ISAC)India 1050612withdrawnMars-Phobos low energy transfer in the restricted three body problemqiaodongDr. Dong QiaoBeijing Institute of TechnologyChina