Distributed Attitude Consensus of Multiple Flexible Spacecraft
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Beschreibung
This book mainly presents the authors' recent studies on the distributed attitude consensus of multiple flexible spacecraft. Modified Rodrigues parameters and rotation matrix are used to represent spacecraft attitude. Several distributed adaptive controllers are presented with theoretical analyses, numerical simulations and experimental verifications. The authors intend to provide a manual that allows researchers, engineers and students in the field of aerospace engineering and mechanics to learn a theoretical and practical approach to the design of attitude consensus algorithms.
This book mainly presents the authors' recent studies on the distributed attitude consensus of multiple flexible spacecraft. Modified Rodrigues parameters and rotation matrix are used to represent spacecraft attitude. Several distributed adaptive controllers are presented with theoretical analyses, numerical simulations and experimental verifications. The authors intend to provide a manual that allows researchers, engineers and students in the field of aerospace engineering and mechanics to learn a theoretical and practical approach to the design of attitude consensus algorithms.
Includes the new results on attitude consensus on SO(3) Considers various actuator and measurement limitations Provides study cases under both undirected and directed graphs
Autor*in
Ti Chen
Themen in »Distributed Attitude Consensus of Multiple Flexible Spacecraft«
Attitude Consensus SO(3) Flexible Spacecraft Adaptive Control Distributed Observer Distributed Attitude Tracking Attitude-Only Measurements Rotation Matrix Actuator Faults
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“Each chapter is endowed with its own reference list. The book strongly relies on the authors’ own experience and can be recommended to researcher in the fields of applied mathematics and flight mechanics and control. With an additional effort it might be useful to graduate students.” (Vladimir Răsvan, zbMATH 1506.70002, 2023)
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