将准最优控制理论用于轨道自主快速交会时线性二次型调节器的设计。
The hypo-optimal theory was applied on the design of linear quadratic regulator for fast and automatic orbit rendezvous in this paper.
本文针对三自由度直升机模型设计了基于线性二次型调节器(LQR)和模糊逻辑的鲁棒控制器。
According to the three degree of freedom (3dof) helicopter model, this paper present a novel robust controler based on LQR and fuzzy theory.
针对倒立摆系统研究了PID、极点配置和线性二次型调节器，并利用MATLAB进行了仿真研究。
PID, pole assignment and linear-quadratic optimal control (LQR) are used to design inverted pendulum systems. And they are researched by MATLAB simulation.
运用改进遗传算法来优化极点配置方法和线性二次型调节器方法的倒立摆控制参数，并取得比较好的仿真效果。
The improved GA is used to optimize the parameters of pole assignment control and LQR control about inverted pendulum systems. And the better simulation results are obtained.
最后，给出了一个线性二次型最优调节器设计实例。
Finally, an example for design of a linear quadratic optimal regulator is given.
线性二次型最优调节器的权矩阵选择问题至今尚未得到较好解决。
The matrices of linear quadratic optimal regulators not yet be resolved perfectively.
线性二次型最优调节器的权矩阵选择问题至今尚未得到较好解决。
The matrices of linear quadratic optimal regulators not yet be resolved perfectively.
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