Slew Control of Prolate Spinners Using Single Magnetorquer
2015; American Institute of Aeronautics and Astronautics; Volume: 39; Issue: 3 Linguagem: Inglês
10.2514/1.g001035
ISSN1533-3884
AutoresJuntian Si, Yang Gao, Abadi Chanik,
Tópico(s)Spacecraft Dynamics and Control
ResumoNo AccessEngineering NoteSlew Control of Prolate Spinners Using Single MagnetorquerJuntian Si, Yang Gao and Abadi ChanikJuntian SiUniversity of Surrey, Guildford, England GU2 7XH, United Kingdom*Ph.D. Candidate, Surrey Space Centre, Faculty of Engineering and Physical Sciences; .Search for more papers by this author, Yang GaoUniversity of Surrey, Guildford, England GU2 7XH, United Kingdom†Professor, Surrey Space Centre, Faculty of Engineering and Physical Sciences; .Search for more papers by this author and Abadi ChanikUniversity of Surrey, Guildford, England GU2 7XH, United Kingdom‡Ph.D. Candidate, Surrey Space Centre, Faculty of Engineering and Physical Sciences; .Search for more papers by this authorPublished Online:30 Nov 2015https://doi.org/10.2514/1.G001035SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About References [1] Raus R., Gao Y. and Watt M., “Review and Analysis of Single-Thruster Attitude Control Algorithms for Spinning Spacecraft,” Proceedings of the International Astronautical Congress, International Astronautical Federation Paper IAC-10-C1-3-7, Prague, Sept. 2010. 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