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State Feedback Control in Equinoctial Variables for Orbit Phasing Applications

2018; American Institute of Aeronautics and Astronautics; Volume: 41; Issue: 8 Linguagem: Inglês

10.2514/1.g003402

1533-3884

Mirko Leomanni, Gianni Bianchini, Andrea Garulli, Antonio Giannitrapani,

Astro and Planetary Science

No AccessEngineering NoteState Feedback Control in Equinoctial Variables for Orbit Phasing ApplicationsMirko Leomanni, Gianni Bianchini, Andrea Garulli and Antonio GiannitrapaniMirko LeomanniUniversity of Siena, 53100 Siena, Italy, Gianni BianchiniUniversity of Siena, 53100 Siena, Italy, Andrea GarulliUniversity of Siena, 53100 Siena, Italy and Antonio GiannitrapaniUniversity of Siena, 53100 Siena, ItalyPublished Online:6 Jun 2018https://doi.org/10.2514/1.G003402SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About References [1] Vallado D. A., Fundamentals of Astrodynamics and Applications, 3rd ed., Springer–Verlag, New York, 2007, Chap. 6. Google Scholar[2] Starek J. A., Açkmeşe B., Nesnas I. 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All rights reserved. All requests for copying and permission to reprint should be submitted to CCC at www.copyright.com; employ the ISSN 0731-5090 (print) or 1533-3884 (online) to initiate your request. See also AIAA Rights and Permissions www.aiaa.org/randp. TopicsAerospace SciencesAstrodynamicsAstronauticsControl TheoryFeedback ControlGuidance, Navigation, and Control SystemsOptimal Control TheoryOrbital ManeuversOrbital PropertySpace Orbit KeywordsLow Thrust ManeuversFeedback Control SystemLinear Quadratic RegulatorGeostationary SatellitesGeostationary Transfer OrbitOrbital EccentricityNumerical SimulationSpace MissionsContinuous Time Algebraic Riccati EquationHighly Elliptical OrbitPDF Received30 October 2017Accepted22 April 2018Published online6 June 2018