推力矢量技术在空空导弹上的应用分析  

The Application Analysis of Thrust Vector Control Systems of Air to Air Missile

作　　者：谢永强[1] 李舜[1] 周须峰[1] 张平[1] 

机构地区：[1]中国空空导弹研究院,洛阳471009

出　　处：《科学技术与工程》2009年第20期6109-6113,共5页Science Technology and Engineering

摘　　要：研究了两种应用于空空导弹的推力矢量技术对导弹总体性能的影响问题。首先建立导弹推力矢量、运动学、动力学以及弹目相对运动数学模型,其次通过导弹性能数字仿真对比分析了两种推力矢量技术的优缺点,最后得到相关研究结论,可为导弹总体设计提供参考依据。The missile overall performance difference between the two-kind thrust vector control systems of air to air missile is studied. The missile kinetic model and the missile kinematic model and the missile TVC model and the target kinematic model are established. By performing the overall performance simulations, the difference between the two-kind thrust vector control systems is presented. The conclusion which is given in the thesis can provide reference on the overall design of air to air missile.

关 键 词：推力矢量 过载 转弯角速率 射程 空空导弹 

分 类 号：V412.4[航空宇航科学与技术—航空宇航推进理论与工程]