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反馈控制器设计
相关语句
  feedback controller design
    Based on the technique of linear matrix inequality (LMI), a new approach of stability analysis and fuzzy state feedback controller design through converting the conditions to the equivalent LMI problems to find the feasible solutions for a set of linear matrix inequalities is proposed.
    提出了采用线性矩阵不等式 ( LMI)方法 ,将该充分条件转化为对线性矩阵不等式族寻求 LMI可行解的凸优化问题 ,得到了稳定性分析和模糊状态反馈控制器设计的新方法。
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  “反馈控制器设计”译为未确定词的双语例句
    The Design of Robust Feedback Controller for a Fighter Aircraft
    歼击机的鲁棒反馈控制器设计
短句来源
    When systems are with multiple time delays, the equivalent inequity for the determination of robust stability of systems is provided, and the design method of robust feedback controller is introduced simultaneously.
    针对含有多个不同滞后时间的系统,给出了一种简明的鲁棒稳定性判别不等式,并根据鲁棒稳定性判据,分别给出了系统含有一个或多个时间滞后的鲁棒反馈控制器设计方法,该方法接近于普通的状态反馈设计,便于工程实现.
短句来源
    According to the relative stability of flight s ta te during aircraft cruising,an efficient way was introduced to design H 2 stati c output feedback controller based on LMI for longitudinal model.
    根据巡航阶段飞机飞行状态相对稳定的特点 ,就飞机纵向通道系统模型 ,基于线性矩阵不等式 (LMI)方法进行具有鲁棒性能的H2 静态输出反馈控制器设计
短句来源
    A LMI(Linear Matrix Inequality)-based method to solve PI output feedback control for aero-engine is presented.
    基于LMI(LinearMatrixInequality,线性矩阵不等式),提出一种航空发动机PI输出反馈控制器设计方法。
短句来源
    The controller for the original plant was derived by means of solving optimal H_∞ dynamic output feedback controller for the generalized plant based on Linear Matrix Inequality (LMI).
    基于LMI(LinearMatrixInequality)方法,对此广义对象进行最优H∞动态输出反馈控制器设计,进而求得原被控对象的控制器。
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  feedback controller design
A dynamic feedback controller design method is proposed for multiple input systems.
      
A new robust discrete time feedback controller design technique, of the sliding mode type, is then proposed for the closed loop regulation of the link position around the prescribed trajectory.
      
Feedback controller design for tracking a single fluorescent molecule
      
Feedback controller design using proportional-integral-derivative (PID), lead-lag or estimator/controller techniques are used for maintaining accurate track following.
      
By constructing piecewise-continuous Lyapunov function for the closed-loop augmented system, we construct the H∞ output feedback controller design procedure as solving a set of bilinear matrix inequalities (BMIs).
      
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This paper deals with the design method of flexible structure low-outhority output rate feed back controller by the theory of matrix perturbation. In the method, the first order eigenvalue perturbation is used to design the controller parameters, the eigenvector perturbation and high order eigenvalue perturabtion are used to construct the design constraint. A simple example indicates that the method is direct and effective.

本文以矩阵特征值、特征向量摄动理论为基础,研究挠性结构低权速率输出反馈控制器的设计。本文的方法是用特征值的一阶摄动设计控制器的参数,用特征向量一阶摄动和特征值高阶摄动规定控制器设计约束。简单的例子表明方法直观有效。

Takagi Sugeno(T S) fuzzy model of flight control systems is established. The sufficient conditions of asymptotic stability and stability with decay rate for the closed loop systems via fuzzy state feedback controller are presented. Based on the technique of linear matrix inequality (LMI), a new approach of stability analysis and fuzzy state feedback controller design through converting the conditions to the equivalent LMI problems to find the feasible solutions for a set of linear matrix inequalities is proposed....

Takagi Sugeno(T S) fuzzy model of flight control systems is established. The sufficient conditions of asymptotic stability and stability with decay rate for the closed loop systems via fuzzy state feedback controller are presented. Based on the technique of linear matrix inequality (LMI), a new approach of stability analysis and fuzzy state feedback controller design through converting the conditions to the equivalent LMI problems to find the feasible solutions for a set of linear matrix inequalities is proposed. Simulation results demonstrate that the approach is valid, and the robustness of control systems is nice.

建立了飞控系统的 Takagi-Sugeno ( T-S)模糊模型 ;给出了设计模糊状态反馈控制器 ,保证闭环系统全局渐近稳定、具有一定衰减率稳定的两个充分条件 ;提出了采用线性矩阵不等式 ( LMI)方法 ,将该充分条件转化为对线性矩阵不等式族寻求 LMI可行解的凸优化问题 ,得到了稳定性分析和模糊状态反馈控制器设计的新方法。仿真结果表明 ,所提出的设计方法方便有效 ,控制器鲁棒性好。

A new robust stability analysis method for time-delay system is presented. Through equivalent transformation of polynomial matrix inequality, the solvable condition for the inequality is obtained. Based on this condition, the robust inequality criterion for time-delay system is simplified and a numerically high efficient algorithm is developed. When systems are with multiple time delays, the equivalent inequity for the determination of robust stability of systems is provided, and the design method of robust...

A new robust stability analysis method for time-delay system is presented. Through equivalent transformation of polynomial matrix inequality, the solvable condition for the inequality is obtained. Based on this condition, the robust inequality criterion for time-delay system is simplified and a numerically high efficient algorithm is developed. When systems are with multiple time delays, the equivalent inequity for the determination of robust stability of systems is provided, and the design method of robust feedback controller is introduced simultaneously. Comparison with other robust analysis methods of time-delay system shows that the new approach is more convenient to implement for both the robust stability analysis and the feedback control design. When all the poles hoped are considered as negative real, only one single value decomposition is needed, and other computational complexity of the new robust controller design is just as the one of ordinary pole assignments. The new algorithm of controller design is suitable to both single and multiple time delay systems.

给出了一种时间滞后系统的鲁棒稳定性分析方法.通过对系统鲁棒稳定条件不等式的变形,得到了该不等式可解的条件,该有解条件不仅大大简化了不等式,而且得到了新的时间滞后系统鲁棒稳定性判据.针对含有多个不同滞后时间的系统,给出了一种简明的鲁棒稳定性判别不等式,并根据鲁棒稳定性判据,分别给出了系统含有一个或多个时间滞后的鲁棒反馈控制器设计方法,该方法接近于普通的状态反馈设计,便于工程实现.飞行控制的实践表明,采用新方法可以得到满意的设计结果.当闭环希望极点选为各不相同的负实数时,鲁棒控制器的设计只需要多进行一次奇异值分解,即可完全等价于人们熟知的极点配置问题.该方法对于含有一个或多个时间滞后的系统都是适用的.

 
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