Fault tolerant attitude control of under-actuated spacecraft: Theory and experiment

This paper investigates fault tolerant attitude control theory and experiment for under-actuated spacecraft with one reaction wheel completely broken and two others suffering actuator faults of partial loss of effectiveness or bias. A non-smooth robust adaptive fault tolerant control law is proposed...

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Veröffentlicht in:	Chinese journal of aeronautics 2023-05, Vol.36 (5), p.465-474
Hauptverfasser:	ZHANG, Zejun, YANG, Hao, JIANG, Bin
Format:	Artikel
Sprache:	eng
Schlagworte:	Actuator fault Air-bearing platform Fault tolerant control Semi-physical experiment Under-actuated spacecraft
Online-Zugang:	Volltext
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