A TSM Control Scheme of Integrated Guidance/Autopilot Design for UAV

摘要：

A scheme for integrated guidance/autopilot design for some UAV based on terminal sliding-mode(TSM) control is proposed. Firstly, the terminal sliding mode control is introduced> then a guidance/control law is designed based on TSM control and the backstepping idea when an integrated guidance/autopilot model on the yaw plane of some UVA is formulated. Secondly, for the unavailable information of the maneuvering target, an estimating method is given and an auxiliary control based on a sliding mode estimator is used to offset the estimation error. Finally, a simulation of some UAV against high maneuvering targets on the yaw plane was made to verify the effectiveness and Tightness of the scheme, and the simulation results have shown that good offensive performance can be got.

关键词： Terminal sliding-mode control Integrated guidance/autopilot design Backstepping

作者: Jinyong Yu Qingjiu Xu Yue Zhi

作者单位: Department of Control Engineering Naval Aeronautical and Astronautical University Yantai,China

会议类型: 国际会议

会议名称: 2011 3rd IEEE International Conference on Computer Research and Development(ICCRD 2011)(2011第三届计算机研究与发展国际会议)

会议地点: 上海

会议语种:英文

页码: 431-435

在线出版日期: 2011-03-11（万方平台首次上网日期，不代表论文的发表时间）