Adaptive Nonsingular Terminal Sliding Mode Control for Attitude Tracking of Spacecraft With Actuator Faults

In this paper, an adaptive nonsingular terminal sliding mode control (ANTSMC) is investigated for attitude tracking of spacecraft with actuator faults. First, a nonsingular fast terminal sliding mode surface is designed to avoid the singularity. Finite-time attitude control is developed using the no...

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Bibliographic Details
Main Authors: Chenghu Jing, Hongguang Xu, Xinjian Niu, Xiaoming Song
Format: Article
Published: IEEE 2019-01-01
Series:IEEE Access
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