Based on the law that the sliding mode of variable structure control is constant to external interference, the thesis designed the output decoupling law of BTT missile.
本文在变结构控制理论对外界扰动的不变性原理的基础上，采用变结构控制方法设计了BTT导弹的输出解耦控制律。
Furthermore, dynamic output feedback variable structure control using outputs of the system and states of the observer is studied.
利用状态观测器的状态及系统输出变量反馈方法，设计了大型空间结构的动态输出变结构控制律。
To solve the attitude maneuver of a flexible satellite, this article presents a variable structure tracking control algorithm based on output feedback.
为解决柔性航天器姿态机动的控制问题，给出了基于输出反馈的变结构跟踪控制算法。
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