高空導彈 的英文怎麼說

中文拼音 [gāokōngdǎodàn]
高空導彈 英文
high-altitude missile
  • 高 : Ⅰ形容詞1 （從下向上距離大; 離地面遠） tall; high 2 （在一般標準或平均程度之上; 等級在上的） above...
  • 空 : 空Ⅰ形容詞（不包含什麼; 裏面沒有東西或沒有內容; 不切實際的） empty; hollow; void Ⅱ名詞1 （天空） s...
  • 導 : 動詞1. （引導） lead; guide 2. （傳導） transmit; conduct 3. （開導） instruct; teach; give guidance to
  • 彈 : 彈名詞1. （彈子; 小球形的東西） ball; pellet 2. （內裝爆炸物, 具有破壞和殺傷能力的東西） bullet; bomb
  • 高空 : high altitude; upper air; welkin高空病 airsickness; altitude sickness; aeroembolism; hypobaropath...
  • 導彈 : guided missile
  1. As a kind of representation of the idea of ncw, the essence of aerial defence missile network - centric operation is to connect every part of the adms within certain areas into a network, in order to utilize and exert the function and advantages of each battle system to the full extent, to shorten the responding time for aerial defence battle system, and thus to improve the whole battle efficiency

    防空導彈網路化作戰是在區域防空作戰背景下研究網路化作戰理論的具體實現，其基本思路是將在一定地域內防空導彈系統的各部分網路化，在通信網路的支持下，充分利用和發揮各作戰系統的功能和優勢，以提高防空作戰系統的反應時間，提高該地域內防空導彈系統的整體作戰效能。
  2. The dynamic performance of a ram air system will vary with mach number and altitude and this tends to follow the aerodynamic characteristics of the missile.

    像導彈空氣動力特性一樣，沖壓空氣式系統的動態特性隨馬赫數和高度的變化而變化。
  3. With the development of science and tecbnology, the electronic warfare has gotten to a new stage, electronic jammers, anti - radialized missiles, superlow altitude attacks have turned into great threats confronted with radar nowadays. former single - based radar not only had difficulty in finishing expected tasks, but also the survival of itself had been a pressing problem, people have to probe into multifarious countermeasures in order to improve the viability and effective work - capacity

    隨著科技的發展，雷達電子戰發展到一個新的階段，電子干擾、反輻射導彈、低空突防和隱身武器已成為當今雷達面臨的四大威脅。傳統的有源雷達不僅很難完成預定的任務，而且自身的生存也成了緊迫問題，人們不得不積極探討各種對策，以提高雷達的生存和有效工作能力。
  4. In the end of this thesis, on the basis of the mathematical model, three segments of trajectory : the vertical turn, the pn guidance and the direct lateral force control in terminal trajectory are simulated. the results show that with the direct lateral force control reduces in terminal trajectory, the miss - distance is reduced and the precision is improved

    4 、論文最後根據前面建立的數學模型，對防空導彈垂直轉彎段、比例導引段以及末端直接力控制段進行了模擬計算，結果表明進行末端直接側向力控制可以有效減小攔截目標時的脫靶量，提高命中精度。
  5. The digital simulation based on this control law denotes that it possesses very well performance, and the interception ability of aam for short range in launching of large off - bore sight angle can be raised

    數字模擬表明，該控制律具有很好的性能，能使近距空空導彈在大離軸角發射時的截擊能力得到提高。
  6. Separation process and signal being sheltered problem for a ground - to - air missile are studied in this paper. in addition, some helpful conclusions that can assist solving practical project problems and improve missile ’ s combat capability are got

    本文以地空導彈為研究對象系統開展分離過程模擬和信號傳輸遮擋分析研究，得到了一些能輔助解決實際工程問題，提高導彈戰鬥力的有益結論。
  7. Today it is one of the most heavily militarised places on earth, a land teeming with tanks, infantry, mobile radars and surface - to - air missiles

    今天，這里是地球上最高度軍事化的地區之一，隨處可見坦克、步兵、移動雷達和地對空導彈。
  8. The achievement of research has been used in design and analysis of experiment result of air defense missile

    研究成果已應用於高速機動防空導彈的設計和試驗結果分析。
  9. For the research requirement of the high g - load mobile missile srm, the work process of solid rocket motor under lateral overload is investigated by the use of theoretical analysis and numerical simulation methods involving the calculation of internal ballistics, the simulation of flow field and the analysis of structural integrity

    本文以高速機動防空導彈固體發動機研製需求為背景，採用理論分析和數值模擬方法，從內彈道計算、內流場模擬、結構完整性分析等幾個方面對橫向過載作用下固體火箭發動機工作過程進行了研究。
  10. In this paper, the backward simulation was summarizd at home andabroad, the characteristics of shell nosing were introduced, the theory and scheme of backward simul - ation of shell nosing was constructed, the determined methods of the boundary conditions were put forward in backward simulation for the processes of shell nosing

    論述了推力矢量控制技術是提高空空導彈性能的核心技術，介紹了常用的三類推力矢量裝置，著重討論了燃氣舵式和擾流片式推矢裝置的特點、設計方法、性能及其優缺點.在此基礎上，研究了適用於氣動力/推力矢量復合控制的變結構控制系統及其開關函數的切換條件和飛行控制系統框圖.最後綜述了推力矢量裝置在第四代空空導彈上的應用情況
  11. Turkey ' s attacks on kurdish targets in northern iraq and russia ' s sale to iran of an anti - aircraft missile system pushed gold and oil prices higher on wednesday

    土耳其對伊拉克北部地區的庫爾德武裝目標發起攻擊，以及俄羅斯向伊朗出售防空導彈系統的消息，推動黃金和原油價格周三雙雙走高。
  12. 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

    摘要目的設計優化一類巡航導彈航跡，且航跡滿足避開地空導彈、高炮、殲擊機群、電磁脈沖等火力單元和地形地物障礙，並且滿足航跡路徑長度短、耗油量少等約束條件。
  13. The kai feng destroyer is belonging to the north china sea fleet, the 109 ship is the tenth ship in the group of type 051 ship. in order to strengthen the battle force, the new type radar and a 8 - tube rattle snake air defense missile launching pad have been equipped on the rear deck

    「開封」號導彈驅逐艦配屬北海艦隊， 109艦是051型導彈驅逐艦系列中的第十艘，該艦為了提高戰斗能力，在艦的尾部裝配了新型的火控雷達和一座8聯裝「響尾蛇」防空導彈發射架，從而提高了防空能力。
  14. Aimed at the fire distribution of the fire command for adg ( air defense group ) made up of agm in the army, a brief analysis of the different point of the shooting beteen anticraft guns and missle and the fire distribution method for adg made up of agm is given, an optimization mathematical model is presented

    針對陸軍彈炮混編防空群射擊指揮中的火力分配問題，簡要分析了防空導彈和高炮武器系統射擊的不同特點，提出了彈炮混編防空群的火力分配方法，並建立了優化火力分配方案的數學模型。
  15. The rafael armament development authority is the national aam house and is currently marketing its python 5 highly agile aam and the activeradar bvr derby

    拉斐爾軍備發展公司是以色列空空導彈研製的官方機構，當前正在出售其怪蛇5型高敏捷空空導彈和主動制導的超視距德比導彈。
  16. To solve the resource problem of anti - missile radar omnidirectional and high data rate tracking targets, missile self - position technology to improve missile position precision based on the scheme of passive bd is put forward

    摘要為了解決近程防空導彈制導雷達實現全方位、高數據率跟蹤多自標、截獲跟蹤多導彈遇到的資源緊張問題，提出了利用bd無源定位方案實現導彈自定位，提高導彈自定位精度的方法。
  17. Abstract : according to the urgent need of anti - cruise missile, a brief ana lysis was made not only on the technical specifications of anti - tbm missile but also on cruise missile infrared characteristics. on the basis of the capabilitie s of low - altitude air - defense missile weapon system using in anti - cruise miss ile, some technical improved approaches have been proposed to enhance the capa bility of anti - cruise missile

    文摘:根據反巡航導彈的迫切需求，進行了反tbm與反巡航導彈技術特點和巡航導彈目標特性的簡要分析，在探討低空防空導彈武器系統反巡航導彈能力的基礎上，提出了一些改進設想和技術途徑，以提高其反巡航導彈能力。
  18. Improving the integrated attacking ability of antiaircraft missile with composite seeker

    採用復合導引頭提高防空導彈綜合打擊能力
  19. 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。
  20. 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。
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