Robust adaptive integrated translation and rotation control of a rigid spacecraft with control saturation and actuator misalignment
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Published:2013-05
Issue:
Volume:86
Page:167-187
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ISSN:0094-5765
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Container-title:Acta Astronautica
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language:en
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Short-container-title:Acta Astronautica
Author:
Zhang Feng,Duan Guangren
Subject
Aerospace Engineering
Reference41 articles.
1. F. Terui, Position and attitude control of a spacecraft by sliding mode control, in: Proceedings of American Control Conference, Philadelphia, Pennsyvania, USA, 1998, pp. 217–221. 2. D.T. Stansbery, J.R. Cloutier, Position and attitude control of a spacecraft using the state-dependent Riccati equation technique, in: Proceedings of American Control Conference, Chicago, Illinois, USA, 2000, pp. 1867–1871. 3. F. Zhang, G. Duan, Robust integrated translation and rotation finite-time maneuver of a rigid spacecraft based on dual quaternion, in: Proceedings of AIAA Guidance, Navigation, and Control Conference, Portland, Oregon, USA, 2011, AIAA 2011–6396. 4. H.Z. Pan, V. Kaplia, Adaptive nonlinear control for spacecraft formation flying with coupled translational and attitude dynamics, in: Proceedings of the Conference on Decision and Control, Orlando, Florida, USA, 2001, pp. 2057–2062. 5. Y, Xu, A. Tatsch, N.G. Fitz-Coy, Chattering free sliding mode control for a 6DOF formation flying mission, in: Proceedings of AIAA Guidance, Navigation, and Control Conference, San Francisco, California, USA, 2005, AIAA 2005–6464.
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