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Model Predictive Control of Spacecraft Relative Motion with Convexified Keep-Out-Zone Constraints

2018; American Institute of Aeronautics and Astronautics; Volume: 41; Issue: 9 Linguagem: Inglês

10.2514/1.g003549

1533-3884

Costantinos Zagaris, Hyeongjun Park, Josep Virgili-Llop, Richard Zappulla, Marcello Romano, Ilya Kolmanovsky,

Dynamics and Control of Mechanical Systems

No AccessEngineering NoteModel Predictive Control of Spacecraft Relative Motion with Convexified Keep-Out-Zone ConstraintsCostantinos Zagaris, Hyeongjun Park, Josep Virgili-Llop, Richard Zappulla II, Marcello Romano and Ilya KolmanovskyCostantinos ZagarisNaval Postgraduate School, Monterey, California 93943, Hyeongjun ParkNaval Postgraduate School, Monterey, California 93943, Josep Virgili-LlopNaval Postgraduate School, Monterey, California 93943, Richard Zappulla IINaval Postgraduate School, Monterey, California 93943, Marcello RomanoNaval Postgraduate School, Monterey, California 93943 and Ilya KolmanovskyUniversity of Michigan, Ann Arbor, Michigan 48103Published Online:22 Jun 2018https://doi.org/10.2514/1.G003549SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About References [1] Lu P., "Introducing Computational Guidance and Control," Journal of Guidance, Control, and Dynamics, Vol. 40, No. 2, 2017, p. 193. doi:https://doi.org/10.2514/1.G002745 JGCODS 0731-5090 LinkGoogle Scholar[2] Tsiotras P. and Mesbahi M., "Toward an Algorithmic Control Theory," Journal of Guidance, Control, and Dynamics, Vol. 40, No. 2, 2017, pp. 194–196. doi:https://doi.org/10.2514/1.G002754 JGCODS 0731-5090 LinkGoogle Scholar[3] Eren U., Prach A., Koçer 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. TopicsControl TheoryFeedback ControlGuidance, Navigation, and Control SystemsOptimal Control TheorySpace Systems and VehiclesSpacecrafts KeywordsLinear Quadratic RegulatorSpacecraftsQuadratic ProgrammingMonte Carlo SimulationFuel ConsumptionAlgebraic Riccati EquationSpacecraft RendezvousMixed Integer Linear ProgrammingResident Space ObjectComputingAcknowledgmentThe authors would like to thank Christopher Petersen for insightful conversations and comments regarding this work.PDF Received3 January 2018Accepted10 April 2018Published online22 June 2018