A composite sliding mode autopilot design

摘要：

Sliding mode control has been applied to the design of many missile autopilots.In this paper,a control method with the primary feedback being proportional to the switching is developed for eliminating the disturbance effect due to model uncertainty.With this control method,a sliding mode autopilot is analyzed.Then,a composite sliding mode control strategy is discussed to reduce the switching frequency.Numerical simulation results show a good performance of the composite control system.

关键词： missile autopilot sliding mode control composite sliding mode model uncertainty.

作者: Qun-li Xia Jing-ju Zhu Zai-kang Qi

作者单位: School of Aerospace Science and Engineering,Beijing Institute of Technology,Beijing,China

会议类型: 国际会议

会议名称: International Conference on Modelling,Identification and Control(模拟、鉴定、控制国际会议)

会议地点: 上海

会议语种:英文

在线出版日期: 2008-06-29（万方平台首次上网日期，不代表论文的发表时间）