摘要
介绍了推力矢量的回转机理和控制种类。通过建立末敏子弹药数学模型,对推力矢量作用力大小、作用时间、作用力持续时间长短与修正距离的关系进行了仿真研究,结果表明利用推力矢量对弹道优化控制是可行的。
The rotary mechanism and control types of thrust vector were in troduced. Simulation study on the relationship between correlted range and force, time, duration time of thrust vector was done through establishing the mathematical model of terminal-sensitive submunition. The results indicate that it is feasible to optimize controlled trajectory by the thrust vector.
出处
《弹箭与制导学报》
CSCD
北大核心
2008年第2期175-176,178,共3页
Journal of Projectiles,Rockets,Missiles and Guidance
关键词
推力矢量
控制弹道
优化
模拟仿真
thrust vector
controlled trajectory
optimization
simulation