程彈道導彈 的英文怎麼說

中文拼音 [chéngdàndàodǎodàn]
程彈道導彈 英文
long range ballistic missile
  • 程 : 名詞1 （規章; 法式） rule; regulation 2 （進度; 程序） order; procedure 3 （路途; 一段路） journe...
  • 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
  • 道 : Ⅰ名詞（道路） road; way; route; path 2 （水流通過的途徑） channel; course 3 （方向; 方法; 道理） ...
  • 導 : 動詞1. （引導） lead; guide 2. （傳導） transmit; conduct 3. （開導） instruct; teach; give guidance to
  • 導彈 : guided missile
  1. Airbm anti - intermediate range ballistic missile

    反中程彈道導彈
  2. This section essence shrinks the proportion is 1 : 43 simulation model vehicle the east wind - 11 short distance trajectory guided missile truck which develops voluntarily by our country, may mobile launch carries the system is a prototype, the chassis and the missile are the alloy manufacture, the missile may take out from the discharger or revolves along with the discharger to each angle, all vehicle doors may open, the rubber tire may rotate, the zero number of articles approaches 200

    此款精縮比例為1 : 43的模擬模型車以我國自行發展、可機動發射的東風- 11短程彈道導彈車載系統為原型，車體及導彈為合金製造，導彈可以從發射架上取出或隨發射架旋轉至各個角度，所有車門均可打開，橡膠輪胎可以轉動，零件數接近200個。
  3. The terminal guidance procedure is simulated, and the results validated the capability of the exoatmosphere kinetic - kill vehicle to hit the target directly

    在此基礎上對動能攔截器的攔截過程進行模擬，驗證了動能攔截器對彈道導彈的直接命中能力。
  4. Trajectory characteristics of hypersonic waverider missile with rocket extended range

    火箭增程乘波外形導彈彈道特性研究
  5. Abstract : solid propellant rocket motors are preferred for most ballistic missiles because they need simple maintenance and can be launched quickly. but the conventional thrust termination devices limit the depletion of every stage ' s grain and increase some extra - weight. an improved method for designing a multi - stage solid rocket based depleted shutdown was provided. in order to solve the problem of lack of thrust termination devices, a device to adjust the burnout angle will match the final burnout velocity and satisfy the desired range. the method can also limit the detection from anti - ballistic missile system

    文摘:由於維護簡單和發射快速，彈道導彈多用固體火箭發動機，但繁雜的推力終止裝置使各級裝藥不能耗盡並讓結構增重.提出了一種對基於耗盡關機多級固體火箭概念設計的改進方法，此方法滿足導彈系統主要的戰技要求.為解決無推力終止裝置的末速不準問題，可在末級發動機採用姿態調整裝置，對射角進行調整，配合末速以滿足射程要求.本方法還可抑制敵方反導探測
  6. The 1972 anti - ballistic missile treaty, defunct since 2002, prohibited the deployment of space - based weapons to shoot down longrange missiles

    1972年的《反彈道導彈條約》 ，從2002年以後失效，該條約禁止部署用於擊落遠程導彈的天基武器。
  7. In this paper, taking the rocket - assisted cartridge as the research object, systematic analyses and studies have been conducted on its ballistics characteristics. the whole ballistics is divided into three stages. different ballistics models and tested data processing methods have been determined according to the different characteristics on each stage

    本文以火箭增程彈為研究對象，在對其彈道特點進行系統的分析研究的基礎上，將全彈道分為三段，根據各段不同的特點導出了不同的彈道模型及測試數據處理方法。
  8. Second, by computing the trajectory of the missile and the method of analyzing cep, influences that the fighter ' s height, speed, pitch angle, the deflection angle between fighter and target, and the target moving characters make on the times of fighter attack and missile launch are deeply developed. third, by relating the motion of the missile and the fighter, the influences that fighter ' s dive angle and the deflection angle between fighter and target make on the attack field of the fighter are discussed in this paper when the fighter perform vertical and horizontal attack. criterion of attack effect is proposed focusing on attack time of the fighter, trajectory of the missile and destruction probability to the target

    本文主要完成了以下幾個方面的工作：對導彈可發射區和飛機可攻擊區進行建模，通過對導彈彈道的模擬計算，並運用典型的圓概率偏差精度分析方法，詳細討論了飛機實施攻擊時，飛機的飛行高度h 、速度v 、俯仰角、與目標的偏離角_ x及目標運動特性等對飛機攻擊時機和導彈發射時機的影響；因此，將飛機和導彈結合起來，詳細研究了飛機在垂直平面和水平平面內實施攻擊時，飛機俯沖角和與目標的偏離角_ x對飛機的攻擊范圍的影響；以飛機實施攻擊的時間t 、彈道特性和對目標的殺傷概率p來評判對地攻擊的效果；最後給出典型算例，通過對空地攻擊過程的模擬實現，對飛機飛行過載提出要求。
  9. The simulation of the terminal guidance procedure is carried out, and the results verified the conclusion that the interceptor can hit the target directly. at last, the effect of flight path angle error on interception performance is analyzed in detail

    在此基礎上進行了動能攔截器攔截過程模擬，驗證了動能攔截器能夠直接碰撞命中彈道導彈的結論，並詳細分析了在不同相對距離的初始條件下，航向誤差對攔截性能的影響。
  10. Last july, north korea sparked international outrage when it test - fired missiles, including a long - range rocket

    去年7月，北韓試射了包括一枚遠程彈道導彈在內的一系列導彈，引起國際憤慨。
  11. Japan ' s top government spokesman says it does not appear that north korea is about to test - fire a long - range ballistic missile

    日本政府首要發言人說，看來北韓不會很快試射一枚遠程彈道導彈。
  12. Last july, north korea sparked international outrage when it test - fired missiles, including a long - range rocket. pyongyang also conducted its first known nuclear test in october

    去年7月，北韓試射了包括一枚遠程彈道導彈在內的一系列導彈，引起國際憤慨。平壤還在去年10月進行了人們所知的第一次核試驗。
  13. Based on the principles of network - centric warfare and the background of anti - ballistic missile operation, the present study describes the process and mission sequence of badms / nco anti - ballistic missile operation, analyses functional modules and functional nodes of badms / nco, designs the functional architecture of badms / nco with a three - layer logic network structure, analyses the components arid functions of three logic networks and their relations

    基於網路中心戰原理，以區域反彈道導彈為背景，描述了混編防空導彈網路化作戰系統反導作戰的作戰過程及其任務序列；分析了混編防空導彈網路化作戰系統的功能模塊和功能節點劃分；構建了以3層邏輯網結構為特徵的混編防空導彈網路化作戰系統功能體系結構，分析了3層邏輯網的組成與功能及其相互關系。
  14. In this paper. the question of compound guidance about mid - long range air - to - air missle to be considered. the main contributions are as follows : first, two midcourse guidance laws are given. that is optimally predictable pn micourse guidance, which is suitable for middle range missle, and singularly perturbed midcourse guidance. which is suitable for long range missle guidance ; then two terminal guidance laws are given. that is variable structure guidance, which is suitable for passive radar guidance. and optimal guidance which is suitable for active radar guidance ; and then the error sourses of hand - off are researched, the hand - off law is given at the time ; fmally, the midcourse guidance laws and terminal guidance laws are tested by simulation, and the whole trajectory simulation are given through hand - off law, and the results are satisfied

    主要工作如下：首先研究了用於中遠程空空導彈復合制導的兩種中制導律，即用於中程導彈的最優預測比例導引中制導律和用於遠程導彈的奇異攝動中制導律，它們均有很好的中制導性能，能夠滿足中末制導的交班要求；接著研究了兩種末制導律，即用於被動雷達末制導的變結構制導律和用於主動雷達導引頭的最優末制導律，均適用於復合制導末制導段；然後分析了中末制導的交班誤差源，討論了用於復合制導的交接律；最後通過模擬，驗證了提出的中制導律和末制導律，結合提出的交接規律，在不同的情況下對中末制導段彈道進行了模擬驗證，結果證明文中提到的中末制導律能夠達到性能指標要求。
  15. Long - range ballistic missile

    程彈道導彈
  16. It has been a important mode in modern war to give a non - contact attack to distant enemy fleetly and accurately, so it becomes the important task of the military power to build national missile defense system of which radar remains the vital sensor

    使用彈道導彈高速精確打擊武器對敵方進行遠程非接觸式空中襲擊，已經成為現代戰爭的一種重要模式，因此構築國家導彈防禦系統成為軍事強國的重要任務，而雷達仍然是這類防禦系統的重要傳感器。
  17. Short - range ballistic missile

    短程彈道導彈
  18. An eati - based analyzing method of system modeling entity oriented was proposed creatively, then a common process of realizing distributing simulation system modeling was expounded by using uml, and at the end, the specific modeling ballistic missile defence simulation system was researched

    摘要提出了一種基於eati面向實體的系統建模分析方法，闡述了利用uml工具實現分散式模擬系統建模的一般過程，然後針對彈道導彈攻防對抗模擬系統這一具體的應用，進行了建模研究。
  19. On the ballistic programming of long - range anti - ship missile

    遠程反艦導彈彈道規劃研究
  20. Medium - range ballistic missile

    中程彈道導彈
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