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In this paper, an adaptive non-singular terminal fault-tolerant controller has been designed for rigid spacecraft attitude maneuver. The proposed controller is based on the sliding mode scheme. An adaptive learning algorithm is applied for the estimation of the uncertainties. The non-singular terminal sliding surface is introduced to guarantee the system states converge to the desired states in finite...
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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