It also discusses the problems of the controllability and observability of the decoupled control systems, and decoupling by output feedback, etc.
同时，还讨论了解耦系统的能控能观测性、输出反馈实现解藕等问题。
Based on the state space model systematized, and applying the dynamic output feedback, the conditions for robustness disturbance decoupling are proposed in the paper.
基于系统的状态空间模型，利用动态输出反馈，给出了鲁棒干扰解耦的条件。
Firstly, the original nonlinear model of the aircraft longitudinal motion is linearized to a three-order decoupling system via the input-output feedback technique.
首先，对飞机纵向运动的非线性模型进行输入输出反馈线性化，将其等效为一个三阶线性系统，并同时实现了解耦。
A comparative study of two decoupling control methods based on vector control and nonlinear multi-input-multi-output state-feedback based on theory of differential geometry is researched.
对异步电动机的矢量控制和基于微分几何理论的非线性多输入多输出状态反馈两种解耦控制方案作理论和试验比较研究。
A comparative study of two decoupling control methods based on vector control and nonlinear multi-input-multi-output state-feedback based on theory of differential geometry is researched.
对异步电动机的矢量控制和基于微分几何理论的非线性多输入多输出状态反馈两种解耦控制方案作理论和试验比较研究。
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