摘要
本文针对末制导炮弹末制导段的运动特点 ,根据控制舵所处位置 ,对脱靶量计算模型进行深入分析 ,并对脱靶量计算公式进行了推导 ,利用末制导炮弹的仿真数据进行了验证 ,得出准确结论 ,对炮弹设计。
Aims at a stady and characterization of the end control segment of an end control shell, based on the position of the control helm. It then analyzes the model for the amount of deviation and its formula,testifies the cause and validates it by an example and draws the credible conclusion. The study will be of value in shell design and in the improvement of testing methods.
出处
《兵工学报》
EI
CAS
CSCD
北大核心
2000年第1期71-74,共4页
Acta Armamentarii
关键词
末制导炮弹
惯性制导
脱靶量
end control shell, inertia control, amount of deviation
