1) robust linear quadratic regulator(RLQR)
鲁棒线性二次型调节器
1.
The design(adopts) a robust linear quadratic regulator(RLQR) controller to improve the system performance due to the external disturbance and system uncertainties.
考虑外部干扰和系统的不确定性,采用鲁棒线性二次型调节器(RLQR)对车辆稳定性进行优化控制,提高系统鲁棒性。
2) linear quadratic regulator(LQR)
线性二次型调节器
1.
A simplified model of the steering system incorporating vehicle dynamics is analyzed based on the structure of the active front steering(AFS) system,and a linear quadratic regulator(LQR) controller is proposed.
并以转向盘转角、横摆角速度和侧偏角为优化目标,设计了线性二次型调节器控制。
3) linear quadratic regulator
线性二次型调节器
1.
Neural network PID control system based on linear quadratic regulators;
基于线性二次型调节器的神经网络PID控制系统
2.
With a DC motor taken as a control object,the DC motor s rotation speed control system is designed with the method of linear quadratic regulator(LQR) of output feedback.
以直流电动机为控制对象,采用输出反馈线性二次型调节器LQR(Linear Quadratic Regu lator)技术完成了直流电动机的转速控制设计。
3.
The optimum control rule is obtained by design of Linear Quadratic Regulator,and the unmeasurable question of open circuit voltage of status variable battery is solved by constructing a status observer to set up a power control algorithm of a fuel cell vehicle based on a full status feedback.
通过设计线性二次型调节器得到最优控制律;通过构造状态观测器解决状态变量蓄电池开路电压不可测量的问题,从而建立了基于全状态反馈的燃料电池汽车动力控制算法。
4) LQR-line quadratic regulator
线性[0]二次型调节器(LQR)
5) linear quadratic regulator(LQR)
线性二次型调节器(LQR)
6) LQR
线性二次型调节器
1.
A SUFFICIENT CONDITION FOR LQR TO STABILIZE SYSTEMS AND ITS APPLICATION TO PREDICTIVE CONTROL;
一种线性二次型调节器闭环稳定的充分条件及在预测控制中的应用
2.
With the helicopter taken as a control ob- ject,a hovering control law,which is made of by a longitudinal control law and a lateral control law,is designed by means of the linear quad- ratic regulator(LQR)of output feedback,making sure that a satisfied helicopter hovering performance is obt.
建立了某型直升机数学模型,并将该模型分解为纵向模型和横侧向模型两部分,提出了悬停控制律应该达到的稳态指标;以该型直升机为被控对象,采用输出反馈线性二次型调节器(LQR)技术设计了由纵向控制律和横侧向控制律组成的悬停控制律,使得直升机能取得满意的悬停性能指标;以该型直升机模型、执行器模型以及设计的悬停控制器构成全数字闭环仿真系统进行控制律仿真验证;仿真结果表明,文中设计的悬停控制律正确有效,能够较好地实现直升机的悬停功能,另外,由于该悬停控制律是基于输出反馈的,在工程上也比较容易实现。
补充资料：输出反馈(见线性二次型次优控制)
输出反馈(见线性二次型次优控制)
output feedback
3h日c卜口fon以以{输出反馈型次优控制。(output王eedbaek)见线性二次
说明：补充资料仅用于学习参考，请勿用于其它任何用途。
参考词条