Nevertheless, the LQR controller can achieve a much better response.
而LQR控制器对于单节桡性臂，则可以较快的达成。
Through the optimization algorithm, the control system with the LQR controller gets very well dynamic and steady state decoupling performance.
通过优化算法，设计出的LQR控制器取得了良好的动、静态解耦效果。
The LQR controller uses the pendulum control mode to keep the pendulum near the vertical up unstable state points and gives signals of car displacement tracking.
LQR控制器用于倒立摆的控制模式，保持摆锤稳定在竖直向上不稳定状态点附近，使小车位移跟踪给定信号。
This paper build a model of hardware in the loop using MATLAB. The linear quadratic optimal control strategy is adopted to design a LQR controller of double inverted pendulum.
本文在MATLAB环境下建立了二级倒立摆的半物理实时仿真模型，并应用线性二次型最优控制策略，设计了一个二级倒立摆lQR控制器。
Then, the expected orientation of spacecraft with zero angular velocity was derived with a new attitude parameterization and LQR controller was designed based on the linearized system.
利用一种新的姿态描述形式推导出了角速度为零时航天器的目标姿态，然后基于线性化后的系统设计了线性二次型最优控制器。
The linear quadratic regulator(LQR) control law is designed for the robust controller of three stabilization axes for a helicopter.
以直升机为被控对象，应用LQR技术设计了三轴稳定鲁棒控制器。
The controller was composed of optimum LQR, fuzzy controller and sliding mode adaptive regulator.
控制器由最优l QR、模糊控制器和滑模自适应调节器组成。
The controller was composed of optimum LQR, fuzzy controller and sliding mode adaptive regulator.
控制器由最优l QR、模糊控制器和滑模自适应调节器组成。
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