在将来，这个机械装置也许会被其他微执行器或者控制策略代替。
This mechanism can be replaced by micro actuators or other control strategies in the future.
控制系统模型包括控制策略、传感器和执行器模型，本文选用的控制策略为PID调节器。
The control system model consists of control strategy, sensors and actuators sub models. The control strategy is a PID controller.
提出了一种基于自适应观测器的故障诊断与容错控制策略，应用到近空间高超声速飞行器(NSHV)上处理执行器故障。
A fault diagnosis and fault-tolerant control scheme using adaptive observer is generalized to near space hypersonic vehicle (NSHV) to deal with actuator fault.
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.
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.
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