H∞ Robust Gain-Scheduled Autopilot Design for Portable Missile

摘要：

An attitude tracking autopilot is designed based on H  robust gain-scheduled technique for the portable missile which is a typical LPV (Linear Parameter Varying)system.The attitude damping loop is treated as controlled plant,and the pitch attitude is fed back directly to be compared with attitude tracking command.This design idea makes the structure of the autopilot simple and the order of the controller lower,which is convenient for practical engineering.Furthermore in order to implement the controller via the missile-borne computer,the discrete form of the attitude tracking controller is presented.Simulation results show the excellent tracking performance and effectiveness of H  robust gain-scheduled tracking autopilot.

作者: CHEN Xianxiang SONG Jianmei

作者单位: Key Laboratory of Dynamics and Control of Flight Vehicle,Ministry of Education,Beijing Institute of Key Laboratory of Dynamics and Control of Flight Vehicle,Ministry of Education, Beijing Institute of

会议类型: 国际会议

会议名称: The 30th Chinese Control Conference(第三十届中国控制会议)

会议地点: 烟台

会议语种:英文

页码: 1-5

在线出版日期: 2011-07-01（万方平台首次上网日期，不代表论文的发表时间）