Adaptive Filtered Backstepping Control for Integrated Missile Guidance and Autopilot

摘要：

　　In this paper,we study integrated guidance and control system considering the input saturation and state constraints for homing missiles.Command filters are exploited in the control design to deal with the state and actuator constraints.And auxiliary systems are introduced into the integrated guidance and control models to analyze the constraint effect.An adaptive law is adopted to compensate unknown uncertainties in the varying-time system.The proposed control scheme guarantees the desired interception performance and the stability of the missile dynamics.And nonlinear 6-DOF simulations are included to demonstrate the effectiveness of our approach.

关键词： Integrated guidance and autopilot input saturation state constraint adaptive backstepping control

作者: LIANG Xiao-Ling HOU Ming-Zhe DUAN Guang-Ren

作者单位: Harbin Institute of Technology,Harbin 150001,P. R. China

会议类型: 国际会议

会议名称: The 33th Chinese Control Conference第33届中国控制会议

会议地点: 南京

会议语种:英文

页码: 2362-2367

在线出版日期: 2014-07-28（万方平台首次上网日期，不代表论文的发表时间）