敏捷导弹气动力/侧向推力复合控制特性分析研究  

Simultaneous lateral thrust and aerodynamic control of an agile missile

作　　者：邹晖[1] 陈万春[1] 王鹏[1] 殷兴良[2] 

机构地区：[1]北京航空航天大学宇航学院,北京100083 [2]中国航天科工集团公司,北京100854

出　　处：《北京航空航天大学学报》2004年第3期192-196,共5页Journal of Beijing University of Aeronautics and Astronautics

摘　　要：讨论了敏捷导弹的气动力与姿控发动机侧向推力复合控制 .提出将控制系统分成控制律和复合逻辑两部分进行设计的方法 ,对敏捷导弹进行复合控制 ,并通过具体的仿真实例比较了在纯气动控制以及姿控发动机在连续和脉冲形式下的控制效果 .The blended control of a tail-controlled agile missile with attitude control motors is discussed. A controller, including aerodynamic control surface and pulse type lateral jets, was developed. It was divided into two parts: the control law and the blend logic. The control law can be designed easily as before, and the blend logic commands the two actuators. Simulations had been carried out to show the performance. Effect of the distance between motors and the center of gravity of the interceptor had also been discussed.

关 键 词：导弹控制 脉冲控制 火箭推力 复合控制 姿态控制 

分 类 号：TJ765.2[兵器科学与技术—武器系统与运用工程]