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- The explicit formula of desired controller was provided by using the solution to the linear matrix inequalities(LMI). 利用线性矩阵不等式(LMI)的解给出了控制器的设计方法。
- And the resilient controllers can be obtained by solving a set of linear matrix inequalities (LMIs). 控制器的设计可以通过求解一组线性矩阵不等式(LMI)得到。
- Linear matrix inequalities (LMI) technique provides a new solution for multi-objective controller synthesis. 线性矩阵不等式(LMI)技术为多目标控制器的综合提供了新的解决途径。
- A new method of applying linear matrix inequalities (LMIs) tomulti-objective eigenstructure assignment is put forward. 提出了将线性矩阵不等式（LMI）技术用于多目标特征结构配置的控制器设计方法。
- On each stage, groups of variables were fixed alternately at the iterations to reduce the NMI to linear matrix inequalities (LMIs). 在每一阶段,每一次迭代过程中,通过交替固定NMI的一个变量,使NMI转变为线性矩阵不等式(LMI)。
- A dynamic feedback compensator synthesis method based on linear matrix inequalities (LMI) and internal model control (IMC) is proposed in this paper. 摘要提出了一种基于线性矩阵不等式(LMI)和内模控制(IMC)的动态反馈抗饱和补偿器的设计方法。
- In addition, a sufficient condition of passivation is provided in terms of linear matrix inequalities with a concrete storage function constructed. 另一方面，将存储函数具体化，利用线性矩阵不等式，推出了广义系统无源的充分条件。
- In this paper, the robust model model predictive control system of polytopic uncertainty was studied by using linear matrix inequalities (LMI). 本文采用线性矩阵不等式(LMI)，研究多模型不确定性描述情况下的鲁棒模型预测控制问题。
- According to the optimal performance and constraint on the control input presented,robust-optimal controller is designed by solving a set of linear matrix inequalities(LMIs). 然后,根据给定的最优性能指标要求以及控制输入约束,通过求解一组线性矩阵不等式(LMIs)进行鲁棒最优控制器设计。
- Based on multiple Lyapunov functions theory, a sufficient condition in form of linear matrix inequalities is derived for the asymptotic stability under arbitrary switching laws. 采用多李雅普诺夫函数法，首先以线性矩阵不等式形式给出了在任意切换信号作用下离散时滞切换系统渐进稳定的一个充分性条件；
- Based on the Lyapunov method, a sufficient condition for the existence of such a state feedback controller is obtained in terms of linear matrix inequalities (LMIs). 基于李雅普诺夫方法，以若干个线性矩阵不等式形式给出了控制器存在的充分条件。
- The schedulability conditions of this system are presented and a dynamic feedback control law is also designed based on linear matrix inequalities (LMIs). 给出了这类系统网络信息的可调度条件，并基于线性矩阵不等式设计动态反馈控制律。
- The existence condition of nonfragile controllers is derived in terms of linear matrix inequalities(LMIs), and the design procedure is formulated as a convex optimization problem. 通过建立和求解一个凸优化问题,给出了非脆弱控制器的设计方法,进而运用提出的方法来控制永磁同步电机混沌系统。
- Based on the theory at Markovian jump linear systems, the sufficient condition of state feedback guaranteed coat canal for networked systems is presented, and the guaranteed cost controller is the solution at a act at linear matrix inequalities. 根据马尔可夫跳变线性系统理论，给出了网络化系统状态反馈保性能控制器存在的充分条件；该保性能控制器为一组线性短阵不等式的解。
- The stability problem is investigated for a class of neutral systems. A stability criterion is obtained in the form of linear matrix inequalities via discretized Lyapunov-Krasovskii functional. 摘要研究了一类中立型系统的稳定性问题，利用离散化的李雅普诺夫泛函，给出了一个稳定性判据条件，所给条件以线性矩阵不等式的形式给出。
- It is shown that L2 gain performance and the control law can be obtained by solving a set of Linear Matrix Inequalities that is numerically feasible with commercially available software. 运用这种方法，系统L2增益控制器设计将转化成求解一组线性矩阵不等式组的可解性问题，可以用软件较方便的求得结果。
- In terms of linear matrix inequalities, sufficient conditions for the solvability of this problem are proposed.The expressions of desired state feedback controllers are also given. 同时以线性矩阵不等式形式给出该问题可解的一个充分条件。
- Based on linear matrix inequalities (LMI) and quantitative feedback theory (QFT), a new design method of aeroengine robust controller was developed for uncertain mathematical model of aeroengine. 针对航空发动机数学模型的不确定性，提出一种基于线性矩阵不等式(LMI)和定量反馈理论(QFT)的航空发动机鲁棒控制器的新的设计方法。
- Based on the sufficient condition and the consideration of an equality constraint, the continuously dynamic output feedback controller was easily constructed for solving linear matrix inequalities. 根据此充分条件，给定一个等式约束，然后通过求解一组线性矩阵不等式，获得了连续动态输出反馈镇定控制器。
- A design method for pre-compensator in frequency domain of aeroengine multivariable control system based on diagonal dominance and the method of linear matrix inequalities (LMI) is presented. 摘要提出了以对角占优为基础，结合线性矩阵不等式进行航空发动机多变量控制系统频域预补偿器的设计。
