Terminal Sliding Mode Control Design for Air-breathing Hypersonic Vehicles

摘要：

A terminal sliding mode controller is designed for a generic air-breathing hypersonic vehicles (AHVs). The model of AHVs is nonlinear, and includes uncertain parameters and intricate coupling between the engine and flight dynamics. An affine form of the longitudinal model is obtained by input/output linearization, and then a controller is designed by using terminal sliding mode method. The terminal sliding mode can make the system stabilize in finite time. Simulation results are provided to show the availability of the designed controller by excellent altitude and velocity tracking performance.

关键词： Terminal sliding mode:Hypersonic:Input/output linearization

作者: Xiaoxiang Hu Changxing Ding Ligang Wu Changhua Hu Hongyi Li Yulin Si Zeguo Wang

作者单位: Space Control and Inertial Technology Research Center,Harbin Institute of Technology,Harbin 150001,P.R.China.X.Hu,and C.Hu are with 302 Unit,Xian Research Institute of High-tech,Xian 710025,P.R.China.

会议类型: 国际会议

会议名称: The 3rd International Symposium on Systems and Control in Aeronautics and Astronautics(第三届航空航天系统与控制国际会议 ISSCAA 2010)

会议地点: 哈尔滨

会议语种:英文

页码: 19-23

在线出版日期: 2010-01-08（万方平台首次上网日期，不代表论文的发表时间）