本文考虑对执行器失效具有完整性的状态反馈律的设计问题。
This paper is concerned with the design of state feedback law which possesses integrity against actuator failures.
针对一类线性时滞不确定系统，研究了在执行器失效情况下的鲁棒容错控制问题。
This paper focuses on the problem of robust fault-control for a class of uncertain time-delay linear systems with actuator failures.
针对挠性航天器执行器卡死与失效故障的姿态稳定控制问题，提出了一种结构简单、计算量小的改进型滑模容错控制策略。
A modified sliding mode fault tolerant controller is developed for flexible spacecraft attitude stabilization control in the presence of loss of actuator effectiveness fault and actuator stuck fault.
考虑到最优反馈控制在部分执行器（传感器）失效时仍能使系统稳定运行的条件，给出了求解该问题的算法，并用实例作了说明。
The effectiveness of this method is proved by simulation results for an anti interference optimal control problem of airborne obstacle avoidance system.
考虑到最优反馈控制在部分执行器（传感器）失效时仍能使系统稳定运行的条件，给出了求解该问题的算法，并用实例作了说明。
The effectiveness of this method is proved by simulation results for an anti interference optimal control problem of airborne obstacle avoidance system.
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