温度对装固体火箭发动机的导弹命中精度的影响及修正

INFLUENCE AND CORRECTION OF TEMPERATURE TO HIT ACCURACY OF THE MISSILE WITH SOLID ROCKET ENGINE

分析了温度对装有固体火箭发动机导弹命中精度的影响。并对某反舰导弹进行大量的弹道计算和分析,得出一种推导计算导引头回调角公式的方法。这一方法同时考虑到温度和飞行时间的修正。

The influence of temperature on hit accuracy of the missile with solid rocket engine is analyzed. A lot of calculation and analysis of trajectory were made for certain missile. The method used to calculate longitudinal correction angle of missile seeker has been got, in consideration of temperature and flight time correction as well.