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 hypo-optimal theory was applied on the design of linear quadratic regulator for fast and automatic orbit rendezvous in this paper.
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。
In this paper, a study on robust stability of linear quadratic regulator (LQR) problem in the case with uncertainties is performed. A new robustness measure is proposed.
本文讨论不确定性系线最优调节器(LQR)的鲁棒稳定性问题，并提出了一种新的评价系统鲁棒稳定性的指标。
The discussion includes linear regulator, state estimator, observer for a linear functional of state, and linear quadratic control with incomplete or noisy measurements.
讨论的问题包括线性调节器，状态估计器，状态线性函数观测器，及不完全或有噪声测量的线性二次控制。
Finally, an example for design of a linear quadratic optimal regulator is given.
最后，给出了一个线性二次型最优调节器设计实例。
This thesis discusses the first-rank control theory which is applied widely, and we discuss the principle and algorithm of linear-quadratic regulator in details.
本设计针对广泛应用的最优控制理论进行论述，并对其在实践中常用的线性二次型问题的原理和算法详细阐述。
On the subject of optimal regulator for a generalized system, if the state trajectories of the system contain some impulses, the corresponding linear-quadratic performance index will become infinite.
关于广义系统的最优调节器问题，如果系统的状态轨迹含有脉冲响应，相应的二次型性能指标为无穷大。
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 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。
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