Affiliation of Author(s):自动化学院
Journal:SEVENTH INTERNATIONAL CONFERENCE ON ELECTRONICS AND INFORMATION ENGINEERING
Key Words:missile maneuver control robust control PI control
Abstract:For the performance of missile with high Mach number and strongly nonlinear dynamics, this paper uses robust control to design maneuver controller. Robust servomechanism linear quadratic regulator (RSLQR) control is used to form the inner loop and proportional-plus-integral (PI) control is used to provide yawing tracking with no error. Contrast simulations under three types of deviation have been done to confirm robustness of the RSLQR-plus-PI control. Simulation results shows that RSLQR-plus-PI control would resist the disturbance and maintain the properties of the controller, guarantee the robustness and stability of missile more effectively than pure PI control.
ISSN No.:0277-786X
Translation or Not:no
Date of Publication:2017-01-01
Co-author:坤娅,Li Chuntao
Correspondence Author:TingZhao
Date of Publication:2017-01-01