Adaptive Sliding Mode Control for Bank-To-Turn Missiles
This paper presents an adaptive sliding mode controller for bank-to-turn (BTT) missiles,which have the characteristics of strong coupling nonlinearity and non-minimum phase phenomenon. From a nonlinear multivariate model of air-to-air missile,a two-loop mathematical model is educed based on singular perturbation theory and time scales. We achieve fin commands for actuators via two-loop adaptive sliding mode control scheme under the assumption that the perturbation is bounded and the guidance commands are given. Moreover,we constitute a sliding mode disturbance observer to estimate the value of perturbation. With the perturbation well estimated,the practicability of the control scheme is guaranteed and the robustness of system is improved. simulation with modeling error and external disturbance shows the validity of the control scheme. Tracking result is highly precise and the angle of sideslip is small,which satisfies the requirement of BTT control.
BTT missiles sliding mode control adaptive control nonlinear control.
Duan Chaoyang Zhang Yingxin Dong Chaoyang Sun Rui
School of Automation Science and Electrical Engineering,Beijing University of Aeronautics and Astron School of Aeronautic Science and Engineering,Beijing University of Aeronautics and Astronautics,Beij
国际会议
2009 9th International Conference on Electronic Measurement & Instruments(第九届电子测量与仪器国际会议 ICEMI2009)
北京
英文
2640-2645
2009-08-16（万方平台首次上网日期，不代表论文的发表时间）