After the coupled process control model was developed, a feedback decoupling controller was proposed to decouple the model.
本文在建立板形板厚耦合模型的基础上，采用反馈解耦控制方法，实现了板形板厚的解耦控制。
A synchronous and disturbance attenuation system for the dual linear servo-motors is designed according to feedback decoupling theory.
运用反馈解耦理论，设计了一个双直线电机的同步抗干扰控制系统。
The paper deals with the decoupling and stable decoupling of non-square systems on the state feedback and input transformation.
本文讨论了非方系统在状态反馈和输入变换下的解耦与稳定解耦的问题。
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。
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。
This paper discusses how to realize the dynamic decoupling of aero engine by state feedback.
利用状态反馈实现了航空发动机的动态解耦。
Moreover, we prove that if the disturbance decoupling problem is solvable by a dynamic state feedback, then it is solvable by a quasi static feedback.
最后证明了：系统可用动态状态反馈解耦，也可通过拟静态状态反馈进行解耦。
In this paper we discuss the disturbance decoupling problem by state feedback for singular systems.
本文讨论利用状态反馈实现奇异系统的干扰解耦问题，提出了绝对C -能观的概念。
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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