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。
Furthermore, dynamic output feedback variable structure control using outputs of the system and states of the observer is studied.
该文给出了系统的状态空间模型、状态观测器的设计方法及估计结果。
In the paper the simulating result and the method of designing state observer and the model of state space is presented.
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.
应用推荐