Sliding Mode Autopilot and Observer Design for a Supersonic Flight Vehicle

摘要：

Design and synthesis of a nonlinear supersonic missile longitudinal dynamics control for angle-of-attack output tracking are presented. In addition a sliding mode observer is designed to estimate the angle-of-attack which is difficult to measure in practice. The employed method is simple to implement in practical applications and enables the sliding mode control design to exhibit the desired dynamic properties during the entire output-tracking process independent of perturbations. Results of simulations are presented to demonstrate the performance, robustness, and stability of the considered autopilot.

作者: M. Bahrami B. Ebrahimi G. R. Ansarifar J. Roshanian

作者单位: Department of Mechanical Engineering,Amirkabir University of Technology,Tehran,Iran;Aerospace Resear Department of Mechanical Engineering,Amirkabir University of Technology,Tehran,Iran Department of Aerospace Engineering,K.N.Toosi University of Technology,Tehran,Iran;Aerospace Researc

会议类型: 国际会议

会议名称: The 2nd International Symposium on Systems and Control in Aeronautics and Astronautics(第二届航空航天系统与控制国际会议 ISSCAA 2008)

会议地点: 深圳

会议语种:英文

页码: 1310-1314

在线出版日期: 2008-12-10（万方平台首次上网日期，不代表论文的发表时间）