In the study of modern control theories, pole assignment and LQR are designed on inverted pendulum systems, and the MATLAB simulation is researched.
利用息现代控制理论，针对倒立摆系统研究了极点配置方法和线性二次型最优控制方法，并利用MATLAB进行了仿真研究。
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。
The simulation results show that, compared with the linear state feedback control (LQR), this system is of fine performance and robustness to different rope lengths.
仿真结果表明了该方法的可行性，与线性状态反馈控制（LQR）相比，该方法对不同的绳长有着较好的鲁棒性。
The running conditions of each part and whole of the system are introduced. Then shaking table test employing LQR classical linear optimal control algorithms is performed.
在详细介绍了系统的各部分与整体运行情况后，采用LQR经典线性最优控制算法对结构进行了振动台试验研究。
By using quadric LQR algorithm, optimal control rule was educed. According to extremum principle, control force of driver on semi-active damper was confirmed.
通过二次型最优控制LQR算法，根据极值原理导出最优控制律，以确定半主动减振器驱动器控制力。
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。
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。
And the vibration power flow transmission optimum control effect is simulated, using the Linear quadratic Regular (LQR) theory.
利用线性二次调节器理论，对耦合系统的振动功率流传递进行了最优控制。
To suppress the simultaneous elastic vibration in movement, an elastic stabilizer is designed by using the LQR control method.
通过最优控制理论设计弹性稳态器，抑制由于刚体运动而激发的弹性振动。
In this paper, the optimal PID control system for aero-engine was designed using LQR (Linear-Quadratic Regulator) approach.
本文采用基于LQR的PID控制算法，设计某型号涡扇发动机控制系统。
In view of the result of simulation, LQR regulation is excellent to the PID control system, LQR regulation accuse as velocity steady controlling in the pump-controlled motor system is better.
从仿真结果上看，LQR调节的性能优与PID控制，说明采用LQR调节器作为泵控马达恒速控制系统的控制方法是良好的。
To solve the problems in pendubot strategy based on partial feedback linearization and LQR, another control strategy based on fuzzy control and LQR is proposed.
基于部分反馈线性化与LQR方法结合的控制策略摇起时间短，控制器之间过渡平稳，但它有成功率不高、参数难调的缺点。
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 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.
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 simulation results show that the results of PID control based on GA are better than experience, but the results of pole assignment control and LQR control are not clear advantage whit experience.
仿真结果表明，基于遗传算法的PID控制效果比经验值要好，但基于遗传算法的极点配置方法和线性二次型最优控制方法的控制效果与经验值相比，没有明显的优势。
The LQR design makes sure the system performance index is satisfied, while the sliding mode control restrains the disturbance exterior, as well as makes sure fast dynamical response.
线性二次型优化设计可以满足系统的静态性能指标要求，而滑模变结构控制抑制了外部干扰的影响，并保证了系统的快速动态响应。
Based on full-car model, an integrated control strategy which consists of filtered LQR and sky-hook damping control is studied.
基于全车模型，其中包括过滤lqr和天勾阻尼控制的综合控制策略进行了研究。
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。
With regard to semi-active control algorithm, a LQR semi-active method, which is based upon classical LQR theory, is put forward in seismie vibration control of Hefei TV tower.
在半主动控制策略方面，运用了两种控制策略：一种是基于最优控制理论的LQR半主动控制策略，另一种是基于局部反馈的模糊半主动控制策略。
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 part of gross scale uses PID to control, and system parameters are provided by LQR;
粗称部分采用PID控制，系统参数由最小二乘法决定；
The active control model and semicontrol model based on the optimal LQR regulator of the pantograph are established.
建立受电弓最优主动控制和最优半主动控制模型；
LQR algorithm USES the least control energy under certain performance index to achieve the smallest state errors.
LQR算法是在特定白勺性能指标下，利用最少白勺控制能量，来到达最小白勺状态误差。
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。
According to the three degree of freedom (3dof) helicopter model, this paper present a novel robust controler based on LQR and fuzzy theory.
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.
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。
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