1) Short distance guidance
近程导引
2) short distance navigation
近距引导
1.
This paper introduces the method of short distance navigation, path characteristics and parameters of fighter plane, presents calculation methods of fighter plane attack envelope and missile launch envelope based on short distance navigation effciency.
介绍了载机近距引导的方法、轨迹 (路径 )特征及参数变化情况 ,给出了基于近距引导效能的飞机攻击区、导弹发射区的计算方法 ,并对一定条件下的近距引导效能进行了分析计算。
3) Introduction to Approximation Theory ?
逼近论导引
4) short range missile
近程导弹
1.
For the short range missile adopting open-loop control flies along the forecast line-of-sight(LOS),the forecast precision determines the missile hit precision.
近程导弹采用预测瞄准线开环控制,瞄准线的预测精度直接决定导弹的命中精度。
5) close-in anti-missile
近程反导
1.
Input and output data are performance index and damage efficiency of different close-in anti-missile naval gun system.
以近程反导舰炮系统的战技术性能指标为输入,毁伤效果为输出,用DEA模型可得系统效性值及各输入性能指标的松弛变量。
6) short range anti-missile
近程反导
1.
Block firing system and multiple hit target in short range anti-missile;
近程反导中拦阻射击模式和多重命中体制研究
补充资料：按摩与导引
按摩与导引
现代中医期刊。广东省中医研究所主办，《按摩与导引》编辑部编。双月刊。发行地广州市。1985年4月创刊。
说明：补充资料仅用于学习参考，请勿用于其它任何用途。
参考词条