Use Roll Actuator to Reduce Coupling of BTT Missile

摘要：

A new structure actuator for reducing coupling of bank-to-turn (BTT) missiles to is studied. The new structure actuator can roll independently along the longitudinal axis of the missile. Hence, the actuator instead of airframe needs to steer when controlling BTT missile rolling. So the rolling speed of main airframe is reduced, it can reduce coupling of missile introduced by airframe rolling. And controlling logic is designed for the missile using roll actuator. Final, analysis and simulation results demonstrate the effectiveness of the rolling actuator in decoupling a BTT missile.

作者: Yu-bin Yu Jing Zhang

作者单位: School of Aerospace Science and Engineering Beijing Institute of Technology Beijing 100081 P.R.China

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: 655-659

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）