Simulation of a Non-fully Recovering LQG/LTR Method
A Non-fully recovering LQG/LTR(Linear Quadratic Gaussian synthesis with Loop Transfer Recovery) method was introduced in the paper for solving the problem of over large values of the parameters in the conventional LQG/LTR controller. After the theory and the approach of Non-fully recovering LQG/LTR were introduced, this method was applied to design the aeroengine control system. The research result showed that the values of Non-fully recovering LQG/LTR controller parameters can be reduced effectively and without any capability loss of the control system compared with the controller designed by conventional LQG/LTR methodology.
Non-fully recovering LQG/LTR Digital Electronic Engine Controller Hardware simulation
Dong Du
Academy of Flight Technology and Safety of Civil Aviation Flight University of China Guanghan, Sichuan Province 618307, China
国际会议
三峡
英文
1037-1040
2012-05-18(万方平台首次上网日期,不代表论文的发表时间)