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Spacecraft Thruster Control via Sigma–Delta Modulation

2017; American Institute of Aeronautics and Astronautics; Volume: 40; Issue: 11 Linguagem: Inglês

10.2514/1.g002986

1533-3884

Richard Zappulla, Josep Virgili-Llop, Marcello Romano,

Stability and Control of Uncertain Systems

No AccessEngineering NoteSpacecraft Thruster Control via Sigma–Delta ModulationRichard Zappulla II, Josep Virgili-Llop and Marcello RomanoRichard Zappulla IINaval Postgraduate School, Monterey, California 93943*Ph.D. Candidate, Mechanical and Aerospace Engineering Department, 1 University Circle. Student Member AIAA.Search for more papers by this author, Josep Virgili-LlopNaval Postgraduate School, Monterey, California 93943†Postdoctoral Research Associate, Mechanical and Aerospace Engineering Department, 1 University Circle. Member AIAA.Search for more papers by this author and Marcello RomanoNaval Postgraduate School, Monterey, California 93943‡Professor, Mechanical and Aerospace Engineering Department, 1 University Circle. Associate Fellow AIAA.Search for more papers by this authorPublished Online:19 Jul 2017https://doi.org/10.2514/1.G002986SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About References [1] Wie B., Space Vehicle Dynamics and Control, 2nd ed., AIAA, Reston, VA, 2008, pp. 77–78, 350–353, 359–361, 425–444, 478–482, 558–574. LinkGoogle Scholar[2] Bernelli-Zazzera F., Mantegazza P. and Nurzia V., “Multi-Pulse-Width Modulated Control of Linear Systems,” Journal of Guidance, Control, and Dynamics, Vol. 21, No. 1, 1998, pp. 64–70. doi:https://doi.org/10.2514/2.4198 JGCODS 0731-5090 LinkGoogle Scholar[3] Curti F., Romano M. and Bevilacqua R., “Lyapunov-Based Thrusters’ Selection for Spacecraft Control: Anlaysis and Experimentation,” Journal of Guidance, Control, and Dyanmics, Vol. 33, No. 4, 2010, pp. 1143–1160. doi:https://doi.org/10.2514/1.47296 LinkGoogle Scholar[4] Song G. and Agrawal B. 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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. TopicsIon ThrusterPropellantPropulsion and PowerSpace Systems and VehiclesSpacecraft PropulsionSpacecrafts KeywordsThrustersSpacecraftsControl Moment GyroscopeClosed LoopAnalog CircuitsFeedback LoopPropellantNumerical SimulationSpacecraft AttitudeFuel ConsumptionAcknowledgmentsThe authors would like to sincerely thank Roberto Cristi for introducing us to the Sigma–Delta modulator in addition to the useful discussion during the course of this work.PDF Received19 April 2017Accepted13 May 2017Published online19 July 2017