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The Attitude Control System (ACS) plays a pivotal role in the whole performance of the spacecraft on the orbit; therefore, it is vitally important to design the control system with the performance of rapid response, high control precision and insensitive to external perturbations. In the first place, this paper proposes two adaptive nonlinear control algorithms based on the sliding mode control (SMC),...
Attitude Control System(ACS) with high performance, high precision, and high reLiabiLity is the kernel technology of the research of spacecraft, which directly affects the whole performance of spacecraft. Hence, a non-singular Terminal adaptive fuzzy sLiding-mode controller is proposed to come true the high performance control. The theory of this controller is to introduce the Limited time mechanics-Terminal...
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