On-orbiting spacecraft are working for a specified long time under the effects of environmental disturbances, uncertainties, component failures, and input saturation.
Finite-Time Fault-Tolerant Spacecraft Attitude Control with Torque Saturation
Control Allocation for Spacecraft Under Actuator Faults ; Kapitel : 5 ; 73-108
2021-03-14
36 pages
Aufsatz/Kapitel (Buch)
Elektronische Ressource
Englisch
Finite-Time Fault-Tolerant Spacecraft Attitude Control with Torque Saturation
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