This paper focuses on the fault-tolerant attitude consensus control (FTACC) for a set of satellites with actuator faults. The attitude dynamical models of the satellites are considered as nonlinear systems, suffering from the effects of parameter variations and environmental uncertainties. A fully distributed attitude control protocol is developed without requirement of global information of the networked spacecraft system. Numerical tests and the results of a set of spacecrafts show the effectiveness of the designed fault-tolerant consensus control protocol.
Distributed Fault-Tolerant Attitude Consensus Control for Multiple Satellites
Lect. Notes Electrical Eng.
International Conference on Guidance, Navigation and Control ; 2022 ; Harbin, China August 05, 2022 - August 07, 2022
2023-01-31
9 pages
Article/Chapter (Book)
Electronic Resource
English
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