The linearquadraticregulator(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。
2
The hypo-optimal theory was applied on the design of linearquadraticregulator 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。
3
In this paper, a study on robust stability of linearquadraticregulator (LQR) problem in the case with uncertainties is performed. A new robustness measure is proposed.