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Combined Nonlinear H∞ Controller for a Controlled-Floating Space Robot

2019; American Institute of Aeronautics and Astronautics; Volume: 42; Issue: 8 Linguagem: Inglês

10.2514/1.g003811

1533-3884

Asma Seddaoui, Chakravarthini M. Saaj,

Silicone and Siloxane Chemistry

No AccessEngineering NotesCombined Nonlinear H∞ Controller for a Controlled-Floating Space RobotAsma Seddaoui and Chakravarthini M. SaajAsma SeddaouiUniversity of Surrey, Guildford, England GU2 7XH, United Kingdom and Chakravarthini M. SaajUniversity of Surrey, Guildford, England GU2 7XH, United KingdomPublished Online:21 Apr 2019https://doi.org/10.2514/1.G003811SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About References [1] Lee N., Backes P., Burdick J., Pellegrino S., Fuller C., Hogstrom K., Kennedy B., Kim J., Mukherjee R., Seubert C. and et al., "Architecture for In-Space Robotic Assembly of a Modular Space Telescope," Journal of Astronomical Telescopes, Instruments, and Systems, Vol. 2, No. 4, 2016, Paper 041207. doi:https://doi.org/10.1117/1.JATIS.2.4.041207 CrossrefGoogle Scholar[2] Reed B. B., Smith R. C., Naasz B. J., Pellegrino J. F. and Bacon C. 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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. TopicsApplied MathematicsElementary AlgebraGeneral PhysicsGeometry FunctionsMathematical AnalysisPlanetary Science and ExplorationPlanetsRiccati EquationsSpace Exploration and TechnologySpace RobotSpace Science and Technology KeywordsFree Flying Space RobotTarget SpacecraftProportional Integral DerivativeFuel ConsumptionDynamically Equivalent ManipulatorReusable Launch VehicleMathematical ModelsAngular MotionEarthSecond Order Differential EquationsAcknowledgmentsThe authors wish to acknowledge the U.K. Space Agency, the Surrey Satellite Technology, Ltd., and the Algerian Space Agency for funding this research.PDF Received8 May 2018Accepted4 March 2019Published online21 April 2019