surface-to-air missile中文是什么意思

• 地对空导弹
• 防空飞弹
• 面对空飞弹
• 面空
• 水面对空导弹

• surface    n. 1.表面；地面；水面；广场，空地。 2.外观，外表 ...
• air    n. 1.空气，大气。 2.天空，空中。 3.微风，和风 ...
• missile    n. 投射器；飞射器[箭、炮弹等]，射弹，飞弹；导弹。 ...
• anti-missile surface-to-air missile    舰对空反导弹导弹
• missile; air-to-surface missile (asm)    空对面飞弹
• air to surface missile    空对地导弹
• air-to-surface aerodynamic missile    空对地飞航式导弹
• air-to-surface ballistic missile    空对地弹道导弹
• air-to-surface missile    空对地导弹; 空对地火箭; 空对面导弹
• air-to-surface missile (asm)    空对地导弹
• air-to-surface missile defense    对空对地导弹的防御
• air-to-surface tactical missile    空对地战术导弹
• counter-air-to-surface missile    反空对空导弹的导弹
• hellfire air-to-surface missile    地狱火空地导弹
• maverick air to surface missile    小牛空对地导弹
• missile; surface-to-air (sam)    面对空飞弹
• surface to air missile    地对空导弹
• surface-to-air ballistic missile    地对空导弹
• surface-to-air missile (sam)    地对空导弹; 面对空飞弹
• surface-to-air missile site    地对空导弹发射场
• surface-to-air-missile    地对空导弹
• tactical air-to-surface missile    战术空对面导弹
• avenger surface to air missile system    地对空导弹系统
• avenger surface-to-air missile system    复仇者”地对空导弹系统
• homing surface to air guided missile    地对空制导导弹

• The short range surface - to - air missiles would be used to protect metropolitan tokyo if interceptors fired from u . s . or japanese ships failed to knock down incoming missiles
  如果从美国或日本军舰上发射的拦截导弹不能击落来袭导弹的话，这些短程地对空导弹将可以用来保护东京大都市地区。
• Russian - made surface - to - air missile , which was owned by a pro - government armed faction , is loaded onto a united nations truck during the launch of a disarmament program in kabul , may 17 , 2004
  5月17日，在阿富汗首都喀布尔举行的解除武装仪式上，一枚原属武装人员的俄制地对空导弹被运上联合国的大卡车。
• A russian - made surface - to - air missile , which was owned by a pro - government armed faction , is loaded onto a united nations truck during the launch of a disarmament program in kabul , may 17 , 2004
  5月17日，在阿富汗首都喀布尔举行的解除武装仪式上，一枚原属武装人员的俄制地对空导弹被运上联合国的大卡车。
• At one time , the paper analyses the main influencing factors to the fire efficiency according the calculated result , and the countermeasures are proposed to improve the operational efficiency of the portable surface - to - air missile resisting the armed helicopter
  同时，结合计算结果分析了影响作战效能发挥的主要因素，提出了提高便携式地空导弹抗击武装直升机作战效能的对策。
• Aim to plan optimal routes for a type of cruise missiles ( cms ) which can avoid the firepower units as surface - to - air missiles , antiaircraft guns , fighter planes , electromagnetism impulse and terrain obstacles and have the shortest length as well as consume the least oil
  摘要目的设计优化一类巡航导弹航迹，且航迹满足避开地空导弹、高炮、歼击机群、电磁脉冲等火力单元和地形地物障碍，并且满足航迹路径长度短、耗油量少等约束条件。
• According to the basic performance indexes of the portable surface - to - air missile and the armed helicopter , the operational effciency of the portable surface - to - air missile resisting the cruise missile is analyzed and calculated with the mathematical analytical method , and deriving the calculate result
  摘要根据便携式地空导弹和武装直升机的基本性能指标，运用数学解析的方法，对某便携式地空导弹抗击武装直升机的作战效能进行了分析计算，并得出计算结果。
• The tactical missile seeker handover accuracy from midcourse to terminal guidance is researched . the small perturbation method is proposed to analyse error sensitivity of the seeker presetting parameters from error sources . firstly , the terminal guidance seeker presetting parameters are computed , based on the equations of a surface - to - air missile movement and a target movement . then the seeker presetting unaccuracy due to the command guidance radar measurement errors is also computed . it can be seen that the seeker presetting errors increase rapidly when the missile is close to the target , which leads to an important conclusion that the late seeker handover from midcourse to teminal guidance should be avoided
  研究复合制导的战术导弹中末制导交班的导引头预定精度问题.提出用小扰动法分析导引头预定参数对误差源的误差敏感性关系.以中远程防空导弹为例，结合导弹运动方程组和目标运动模型，计算了中末制导交班的导引头预定参数，并计算了在制导站雷达测量误差下的末制导导引头预定参数的计算精度.可知，导引头定位参数的计算误差随着弹目距离的接近而显著增大，得到中末制导交班不能太晚的重要结论
• Abstract : the tactical missile seeker handover accuracy from midcourse to terminal guidance is researched . the small perturbation method is proposed to analyse error sensitivity of the seeker presetting parameters from error sources . firstly , the terminal guidance seeker presetting parameters are computed , based on the equations of a surface - to - air missile movement and a target movement . then the seeker presetting unaccuracy due to the command guidance radar measurement errors is also computed . it can be seen that the seeker presetting errors increase rapidly when the missile is close to the target , which leads to an important conclusion that the late seeker handover from midcourse to teminal guidance should be avoided
  文摘:研究复合制导的战术导弹中末制导交班的导引头预定精度问题.提出用小扰动法分析导引头预定参数对误差源的误差敏感性关系.以中远程防空导弹为例，结合导弹运动方程组和目标运动模型，计算了中末制导交班的导引头预定参数，并计算了在制导站雷达测量误差下的末制导导引头预定参数的计算精度.可知，导引头定位参数的计算误差随着弹目距离的接近而显著增大，得到中末制导交班不能太晚的重要结论
• With the development of science , new method is used in fighter plane and missile design , and new material is used in fighter plane and missile production , which make them have higher speed , higher maneuvering , smaller radar cross section and better jamming and anti - jamming ability . all these development is a big challenge to surface - to - air missile and makes the battlefield environment more complicated
  随着科技的进步,新技术、新材料的大量应用,使作战飞机和战术导弹具有更快的飞行速度,更好的机动性能以及更小的雷达反射面积;同时,电子对抗技术的广泛使用,这些都给防空导弹带来了巨大挑战,使地面防空变得日趋复杂。

• surface-to-air missileとは意味：地対空｛ち たい くう｝ミサイル◆【略】SAM