Title :
H∞ controller design of a missile guidance and control system
Author :
Wang, Jianwei ; Xie, Xueshu ; Zhong, Yisheng ; Wang, Borong
Author_Institution :
Dept. of Autom., Tsinghua Univ., Beijing, China
Abstract :
Presents a case study of H∞ robust controller design of the guidance and control system of an air-to-air missile. Simulations of a simplified linear time-invariant model and a nonlinear time-varying six degree-of-freedom model indicate that the guidance and control system with an H∞ controller can achieve better performance and robustness than that with a proportional navigation amplifier without changing of any other components in the system
Keywords :
H∞ control; control system synthesis; linear systems; missile guidance; nonlinear control systems; robust control; time-varying systems; H∞ robust controller; air-to-air missile; missile guidance and control system; nonlinear time-varying six degree-of-freedom model; simplified linear time-invariant model; Acceleration; Automatic control; Control system synthesis; Control systems; Mathematical model; Missiles; Navigation; Proportional control; Robust control; Virtual manufacturing;
Conference_Titel :
American Control Conference, 1997. Proceedings of the 1997
Conference_Location :
Albuquerque, NM
Print_ISBN :
0-7803-3832-4
DOI :
10.1109/ACC.1997.611961
