This paper considers the problem of attitude tracking control for uncertain rigid spacecraft subject to control input magnitude and rate saturation (MRS). First, a smooth input MRS model is proposed. Then, a robust attitude tracking control scheme is designed based on the backstepping and finite-time disturbance observer techniques. Finally, the effectiveness of the control scheme derived here is illustrated by numerical simulations.
Disturbance Observer-Based Attitude Control for Spacecraft With Input MRS
IEEE Transactions on Aerospace and Electronic Systems ; 55 , 1 ; 384-396
2019-02-01
3684084 byte
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
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