Launch Vehicle Pitch Control via GPI Observer-based Sliding Mode Technique

摘要：

This paper proposes a sliding mode control method, which is combined with the generalized proportional-integral (GPI) observer. The GPI observer has been proved to be asymptotically convergent. The GPI observer-based sliding mode control can eliminate the chattering which is the drawback of the sliding mode control. The stability analysis of the present method is given in this paper. The disturbance rejection capability of the proposed method ensures quickly reference trajectory tracking. The obtained results are exemplified through simulations of a nonlinear system and a launch vehicle application.

关键词： GPI Observer Sliding mode control Chattering elimination

作者: OU Liuli ZHAO Dangjun WANG Yongji LIU Lei

作者单位: Department of Control Science and Engineering, Huazhong University of Science and Technology, Wuhan School of Aeronautics and Astronautics, Central South University, Changsha 410083

会议类型: 国际会议

会议名称: The 31st Chinese Control Conference(第三十一届中国控制会议)

会议地点: 合肥

会议语种:英文

页码: 3166-3170

在线出版日期: 2012-07-01（万方平台首次上网日期，不代表论文的发表时间）