摘要
建立了以不同时滑离方式发射的火箭的仿真模型 ,对某气象火箭在考虑下沉角及下沉角速度时的飞行轨迹进行了数值仿真。计算结果表明 :下沉角及下沉角速度对气象火箭射高有一定影响。
The simulation model of a rocket with sinking motion on the launching rail is established. The flight path of a meteorological rocket is numerical simulated considering sinking angle and sinking angle velocity. The calculation results show that sinking angle and sinking angle velocity have some effect on the overall height of meteorological rocket.
出处
《弹箭与制导学报》
CSCD
北大核心
2002年第2期58-59,63,共3页
Journal of Projectiles,Rockets,Missiles and Guidance
关键词
下沉角
速度
气象火箭
仿真
离轨模型
sinking angle
sinking angle velocity
meteorological rocket
simulation
