Study on Dynamic Decoupling Design by Using INA Method for Cruise Missile

摘要：

The non-square model of cruise missile is strongly coupled between roll and yaw channels when the autopilot is design. Multi-variables coupling analysis is completed with a directive gain matrix for the non-square system. Then the non-square system is squared with coupling analysis and inner feedback. An extended dynamic decoupling method by using INA is presented for a dynamic pre-compensator design of a cruise missile non-square system. The mathematical simulation results indicate that the coupling effect is obviously weaken after using the dynamic decoupling compensator and drive a conclusion that the method is valid.

作者: XU. Jiangtao CUI. Naigang TIAN. Jichao LIU. Hongliang

作者单位: Dept.of astronautic Engineering,Harbin institute of Technology Centre for Control Theory and Guidance Technology,Harbin institute of Technology P.O.Box345,Harbin 1

会议类型: 国际会议

会议名称: The 2nd International Symposium on Systems and Control in Aeronautics and Astronautics(第二届航空航天系统与控制国际会议 ISSCAA 2008)

会议地点: 深圳

会议语种:英文

页码: 1381-1385

在线出版日期: 2008-12-10（万方平台首次上网日期，不代表论文的发表时间）