surface to air missile 中文意思是什麼

surface to air missile 解釋
地對空導彈
  • surface : n 1 表面；地面；水面；廣場，空地。2 外觀，外表，皮毛。3 【幾】面；切口；【航空】翼面。adj 表面的...
  • to : adv 到某種狀態；〈特指〉到停止狀態；關閉。 ★也常和動詞結合，略去其後賓語，而構成成語： The door i...
  • air : n 1 空氣，大氣。2 天空，空中。3 微風，和風。4 態度，樣子，風度，氣派；〈pl 〉高傲的架子。5 傳播，...
  • missile : n 投射器；飛射器[箭、炮彈等]，射彈，飛彈；導彈。 an air to air （guided） missile 空對空飛彈，機...
  1. Avenger surface - to - air missile system

    地對空導彈系統
  2. The standardization of surface to air missile firepower unit mainly resolves the complicacy of the surface to air missile

    摘要地空導彈火力單元作戰效能標準化主要解決地空導彈型號的復雜性問題。
  3. Analysis and study on combat effectiveness of air - to - surface cruise missile

    空地巡航導彈作戰效能的分析研究
  4. The air defence system is the simbad twin missile launcher for the mistral surface - to - air missile, supplied by mbda ( formerly matra bae dynamics, france )

    導彈防空力量為二聯裝法制西北風地對空導彈，發射裝置布局在船位。
  5. Norwegian advanced surface - to - air missile system nasams

    挪威先進面對空導彈系統
  6. Based on analysis of the concept and requirement of low cost surface to air missile, the cost composition and sensitive factors of surface to air missile weapon system were explored, and the feasibility and necessity for achieving low cost and its relationship with the armament system construction were investigated

    摘要在分析低成本防空導彈概念和需求的基礎上，探討了防空導彈武器系統的成本分解結構和對成本價格的敏感因素，研究了實現低成本的可行性、必要性及其與陸軍防空裝備體系建設的關系。
  7. The combat efficiency of the surface to air missile firepower unit is standardized based on the index proportion and efficiency index, and that is a scientific method for the combat efficiency standardization of surface to air missile firepower unit

    在運用層次分析法計算權重，採用混合計演算法計算效能指數的基礎上對地空導彈火力單元的作戰效能進行標準化，為地空導彈火力單元作戰效能的標準化提供了一種科學方法。
  8. Other weapons on display in beijing are the j11b multifunction fighter, new generation 99g main battle tank ( mbt ), type 97 infantry fighting vehicle ( ifv ), hq9 long range surface - to - air missile ( sam ), and new 155mm self - propelled gun ( spg ), similar to the russian 2s19 spg

    在北京的在展覽上的其他的武器是j11b多功能鬥士，新的第99代g主要的戰爭儲于槽中（ mbt ） ，鍵入97個步兵戰斗車輛（ ifv ） ， hq9渴望范圍地對空導彈（山姆） 、和新的155毫米自力推進的槍（運動游戲） ，類似俄國2個s19運動游戲。
  9. Amsam anti - missile surface - to - air missile

    地對空反導彈導彈
  10. As a result, a friendly surface - to - air missile was mistakenly fired at us

    結果，自動瞄準的地對空導彈誤中了我們。
  11. Study on decision support system of the inventory of spare parts for surface - to - air missile weapon system

    防空導彈武器系統備件儲存量決策支持系統研究
  12. After 75 combat missions, his plane was destroyed by a surface - to - air missile. plumb ejected and parachuted into enemy hands. he was captured and spent six years in a communist vietnamese prison

    在完成了七十五次戰役任務后，他的飛機被一枚地對空飛彈擊毀，帕朗柏跳傘逃命，卻降落在敵方陣營里，他被越共俘虜並被關在監獄里六個月，之後，他從這場苦難中成功逃生。
  13. And then based on a surface - to - air missile that satisfies the requisition nearly, by means of reconstructing its geometry size, subsystems such as engine, the interceptor model used to continue the following studies is established. then the trajectory - control jet or attitude - control jet is added to the interceptor based on the analysis of the relationship between the missile performance and the thrust and configuration of the side jet

    然後以基本滿足方案要求的某型防空導彈為基礎，對其幾何尺寸、發動機等分系統進行改進，並通過分析導彈性能與側噴發動機參數之間的關系，增加了姿控或軌控側向裝置，這樣得到了本文的研究工作所需的導彈模型。
  14. 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

    同時，結合計算結果分析了影響作戰效能發揮的主要因素，提出了提高便攜式地空導彈抗擊武裝直升機作戰效能的對策。
  15. Study on the model of intercepting decision for multi channel surface to air missile weapon system

    多通道地空導彈武器系統攔截決策模型研究
  16. The fuzzy synthetic evaluation of the operational effectiveness of the guided surface to air missile

    模糊綜合評判地空導彈武器系統作戰效能的一種方法
  17. Abstract : sins initial alignment error is one of the important error sources for tactical surface to air missile precision allocation. it is necessary and advantageous to research quickly separate technique of sins initial alignment error in outfield for improving missile guidance precision

    文摘:捷聯慣性導航系統的初始對準誤差是戰術地空導彈精度分配中的主要誤差源之一，研究在外場條件下初始對準誤差的快速分離方法對于提高導彈制導精度具有積極意義。
  18. 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

    隨著科技的進步，新技術、新材料的大量應用，使作戰飛機和戰術導彈具有更快的飛行速度，更好的機動性能以及更小的雷達反射面積;同時，電子對抗技術的廣泛使用，這些都給防空導彈帶來了巨大挑戰，使地面防空變得日趨復雜。
  19. 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

    研究復合制導的戰術導彈中末制導交班的導引頭預定精度問題.提出用小擾動法分析導引頭預定參數對誤差源的誤差敏感性關系.以中遠程防空導彈為例，結合導彈運動方程組和目標運動模型，計算了中末制導交班的導引頭預定參數，並計算了在制導站雷達測量誤差下的末制導導引頭預定參數的計算精度.可知，導引頭定位參數的計算誤差隨著彈目距離的接近而顯著增大，得到中末制導交班不能太晚的重要結論
  20. 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:研究復合制導的戰術導彈中末制導交班的導引頭預定精度問題.提出用小擾動法分析導引頭預定參數對誤差源的誤差敏感性關系.以中遠程防空導彈為例，結合導彈運動方程組和目標運動模型，計算了中末制導交班的導引頭預定參數，並計算了在制導站雷達測量誤差下的末制導導引頭預定參數的計算精度.可知，導引頭定位參數的計算誤差隨著彈目距離的接近而顯著增大，得到中末制導交班不能太晚的重要結論
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