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| 敏捷导弹气动力/侧向推力复合控制特性分析研究 | |
| 引用本文： | 邹晖,陈万春,王鹏,殷兴良.敏捷导弹气动力/侧向推力复合控制特性分析研究[J].北京航空航天大学学报,2004,30(3):192-196. |
| 作者姓名： | 邹晖 陈万春 王鹏 殷兴良 |
| 作者单位： | 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 |
| 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.最后分析了姿控发动机到拦截器质心的距离对控制效果的影响. |
| 关 键 词： | 导弹控制 脉冲控制 火箭推力 复合控制 姿态控制 |
| 文章编号： | 1001-5965(2004)03-0192-05 |
| 收稿时间： | 2002-11-29 |
| 修稿时间： | 2002年11月29日 |
Simultaneous lateral thrust and aerodynamic control of an agile missile |
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| Zou Hui,Chen Wanchun,Wang Peng,Yin Xingliang.Simultaneous lateral thrust and aerodynamic control of an agile missile[J].Journal of Beijing University of Aeronautics and Astronautics,2004,30(3):192-196. | |
| Authors: | Zou Hui Chen Wanchun Wang Peng Yin Xingliang |
| Institution: | 1. School of Astronautics, Beijing University of Aeronautics and Astronautics， Beijing 100083, China; 2. China Aerospace Science and Industry Corp, Beijing 100854, China |
| Abstract: | 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 been also discussed. |
| Keywords: | guided missile control impulse control rocket thrust blended control attitude control |
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