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发表刊物：Acta Astronautica
关键字：Flexible spacecraft Attitude and angular velocity stabilization Actuator complete failure
摘要：This paper considers the attitude and angular velocity stabilization problem of a class of flexible spacecraft under actuator complete failure. Firstly a new model simplification strategy is put forward to weaken the coupling effects. Then an adaptive observer-based estimation method is proposed to estimate the uncertainty of flexibility, based on which a feedback fault-tolerant control scheme is further developed which guarantees the system stability and asymptotic attitude converging properties. The simulation results illustrate the efficiency of the theoretical results.
卷号：123
页面范围：129-136
是否译文：否
发表时间：2016-07-13
收录刊物：EI
合写作者：Bin Jiang,Liyan Wen
通讯作者：Hao Yang