In practical applications, the external disturbances and uncertainties are always exist for the spacecraft attitude control system.
Extended State Observer Based Optimal Attitude Robust Control of Spacecraft
Control Allocation for Spacecraft Under Actuator Faults ; Kapitel : 6 ; 109-131
14.03.2021
23 pages
Aufsatz/Kapitel (Buch)
Elektronische Ressource
Englisch
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