A Maneuver Controller with Disturbance Attenuation for Aircraft

摘要：

In this paper, a maneuver controller for a nonlinear six-degree-of-freedom aircraft is designed, which makes angle-of-attack, sideslip angle, and roll rate asymptotically track the reference trajectories respectively. The design procedures for angle-of-attack and sideslip angle are based on backstepping method. Appropriate cost functions for angle-ofattack and sideslip angle are constructed to satisfy Hamilton Jacobi-Isaacs (HJI) equations, thereby the tracking of the angleof attack and the sideslip angle attains a desired disturbance attenuation level. Simulation results on a nonlinear aircraft model are given to illustrate the performance of the maneuver controller.

作者: Ruyi Yuan Jianqiang Yi Guoliang Fan Wensheng Yu Liwei Qiu

作者单位: Institute of Automation,Chinese Academy of Sciences,Beijing,China Institute of Automation,Chinese Academy of Sciences,Beijing,China;Shanghai Key Laboratory of Trustwo

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: 727-732

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）