Adaptive Sliding Mode BTT Autopilot for Cruise Missiles with Variable-Swept Wings

作     者：Wei-Ming Li Rui-Sheng Sun Hong-Yang Bai Peng-Yun Liu 

作者机构：School of Energy and Power EngineeringNanjing University of Science and Technology 

出 版 物：《Journal of Harbin Institute of Technology(New Series)》 (哈尔滨工业大学学报（英文版）)

年 卷 期：2014年第21卷第2期

页      面：33-42页

核心收录：

学科分类：08[工学] 0825[工学-航空宇航科学与技术] 

基　　金：Sponsored by the National Natural Science Foundation of China(Grant No.11176012) Aviation Science Foundation of China(Grant No.20110159001) 

主　　题：BTT autopilot adaptive sliding mode control variable-sweep wing 

摘      要：In this paper,an adaptive sliding mode method was proposed for BTT autopilot of cruise missiles with variable-swept wings. To realize the whole state feedback,the roll angle,normal overloads and angular rates were considered as state variables of the autopilot,and a parametric sliding mode controller was designed via feedback linearization. A novel parametric adaptation law was put forward to estimate the nonlinear timevarying parameter perturbations in real time based on Lyapunov stability theory. A sliding mode boundary layer theory was adopted to smooth the discontinuity of control variables and eliminate the control chattering. The simulation was presented for the roll angle and overload commands tracking in different configuration schemes. The results indicated that the controlled system has robust dynamic tracking performance in condition of the large-scale aerodynamic parametric variety resulted from variable-swept wings.