Adaptive back-stepping sliding mode attitude control of missile systems

作者：Xia, Yuanqing^*; Lu, Kunfeng; Zhu, Zheng; Fu, Mengyin

来源：International Journal of Robust and Nonlinear Control, 2013, 23(15): 1699-1717.

DOI：10.1002/rnc.2952

• sliding mode control
• back-stepping
• adaptive control
• missile attitude control

This paper is devoted to the attitude control of a quaternion missile model, which is nonlinear in aerodynamics with atmospheric moment uncertainties, inertia uncertainties, bounded disturbances and actuator failures. By employing the back-stepping technique, the corresponding sliding mode controller is designed to guarantee the state variables of the closed loop system to converge to a small region of the reference states with the help of the adaptive law by estimating the total uncertainties, and be chatter-free. Also, simulation results are presented to illustrate the effectiveness of the control strategy.

• 出版日期2013-10
• 单位北京理工大学