Adaptive control for missile systems with parameter uncertainty

作者：Lin Zhiwei^*; Zhu Zheng; Xia Yuanqing; Wang Shuo

来源：ICIC Express Letters, 2010, 4(5 B): 1937-1944.

• Adaptive control
• Back-stepping
• Missile attitude Control
• Sliding mode control

This paper is devoted to attitude control of a nonlinear missile model. Combining the back-stepping technique, the corresponding sliding mode controller is designed to guarantee the state variables of the closed loop system to converge to the reference state with the help of the adaptive law by estimating the total uncertainties. Also, simulation results are presented to illustrate the effectiveness of the control strategy.

• 出版日期2010
• 单位北京理工大学