Title :
Nonlinear backstepping control of reentry warhead with hybrid actuators
Author :
Wang Zhen ; Wu Zhong
Author_Institution :
Sch. of Instrum. Sci. & Opto-Electron. Eng., Beijing Univ. of Aeronaut. & Astronaut., Beijing, China
Abstract :
A novel set of hybrid actuators with single control moment gyoscopes(SGCMGs) and moving masses are proposed to control a reentry warhead attitude, Since the hybrid actuators are both mounted inside the warhead directly, the ablation of them can be prevented and the aerodynamic shape can be preserved. Considering of the nonlinear and strong coupling characteristic of the reentry warhead dynamic model, A nonlinear attitude control system is designed based on backstepping method which has structured and systematic advantages. This controller has strong robustness, can achieved the two-loop control of the warhead attitude angular velocity and attitude angle. Simulation results demonstrate that the attitude controller has a high control precision and is effective.
Keywords :
actuators; aerodynamics; aircraft control; angular velocity control; attitude control; explosives; gyroscopes; military aircraft; nonlinear control systems; vehicle dynamics; SGCMG; ablation; aerodynamic shape; backstepping method; hybrid actuators; moving masses; nonlinear attitude control system; nonlinear backstepping control; nonlinear coupling characteristic; reentry warhead attitude control; reentry warhead dynamic model; single control moment gyoscopes; strong coupling characteristic; two-loop warhead attitude angle control; two-loop warhead attitude angular velocity control; Actuators; Aerodynamics; Attitude control; Backstepping; Educational institutions; Electronic mail; Vehicle dynamics; Backstepping Control; Control moment gyroscopes; Moving Mass; Nonlinear; Reentry warhead;
Conference_Titel :
Control Conference (CCC), 2012 31st Chinese
Conference_Location :
Hefei
Print_ISBN :
978-1-4673-2581-3