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CubeSat Adaptive Attitude Control with Uncertain Drag Coefficient and Atmospheric Density

2020; American Institute of Aeronautics and Astronautics; Volume: 44; Issue: 2 Linguagem: Inglês

10.2514/1.g005515

1533-3884

Runhan Sun, Camilo Riano-Rios, Riccardo Bevilacqua, Norman Fitz-Coy, Warren E. Dixon,

Adaptive Control of Nonlinear Systems

No AccessEngineering NotesCubeSat Adaptive Attitude Control with Uncertain Drag Coefficient and Atmospheric DensityRunhan Sun, Camilo Riano-Rios, Riccardo Bevilacqua, Norman G. Fitz-Coy and Warren E. DixonRunhan SunUniversity of Florida, Gainesville, Florida 32603, Camilo Riano-RiosUniversity of Florida, Gainesville, Florida 32603, Riccardo BevilacquaUniversity of Florida, Gainesville, Florida 32603, Norman G. Fitz-CoyUniversity of Florida, Gainesville, Florida 32603 and Warren E. DixonUniversity of Florida, Gainesville, Florida 32603Published Online:29 Dec 2020https://doi.org/10.2514/1.G005515SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About References [1] Bevilacqua R. and Romano M., "Rendezvous Maneuvers of Multiple Spacecraft Using Differential Drag Under J2 Perturbation," Journal of Guidance, Control, and Dynamics, Vol. 31, No. 6, 2008, pp. 1595–1607. https://doi.org/10.2514/1.36362 LinkGoogle Scholar[2] Guglielmo D., Omar S., Bevilacqua R., Fineberg L., Treptow J., Poffenberger B. and Johnson Y., "Drag Deorbit Device: A New Standard Reentry Actuator for CubeSats," Journal of Spacecraft and Rockets, Vol. 56, No. 1, 2019, pp. 129–145. https://doi.org/10.2514/1.A34218 LinkGoogle Scholar[3] Omar S. 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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 eISSN 1533-3884 to initiate your request. See also AIAA Rights and Permissions www.aiaa.org/randp. TopicsAerodynamicsAeronautical EngineeringAeronauticsAerospace SciencesAstrodynamicsAstronauticsAtmospheric ScienceAttitude ControlOrbital ManeuversOrbital PropertySatellitesSpace OrbitSpace Systems and VehiclesSpacecraft Attitude ControlSpacecrafts KeywordsAtmospheric DensityAerodynamic TorqueCubeSatAttitude StabilizationQuaternionsYawAdaptive Control MethodAttitude TrackingEarthAtmospheric DragAcknowledgmentsThis research is supported in part by the Air Force Office of Scientific Research award number FA9550-19-1-0169 and the Fulbright Colombia Commission. Any opinions, findings, and conclusions or recommendations expressed in this material are those of the authors and do not necessarily reflect the views of the sponsoring agency.PDF Received6 July 2020Accepted17 November 2020Published online29 December 2020