進攻性導彈 的英文怎麼說

中文拼音 [jìngōngxìngdǎodàn]
進攻性導彈 英文
aggressive missile
  • : 進構詞成分。
  • : Ⅰ動詞1 (攻打) attack; assault; take the offensive 2 (指責別人的過錯; 駁斥別人的議論) accuse; ...
  • : Ⅰ名詞1 (性格) nature; character; disposition 2 (性能; 性質) property; quality 3 (性別) sex ...
  • : 動詞1. (引導) lead; guide 2. (傳導) transmit; conduct 3. (開導) instruct; teach; give guidance to
  • : 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
  • 進攻性 : offensive
  • 進攻 : attack; assault; offensive
  • 導彈 : guided missile
  1. 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:對可發射區和飛機可擊區行建模,通過對道的模擬計算,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及目標運動特等對飛機擊時機和發射時機的影響;因此,將飛機和結合起來,詳細研究了飛機在垂直平面和水平平面內實施擊時,飛機俯沖角和與目標的偏離角_ x對飛機的擊范圍的影響;以飛機實施擊的時間t 、道特和對目標的殺傷概率p來評判對地擊的效果;最後給出典型算例,通過對空地擊過程的模擬實現,對飛機飛行過載提出要求。
  2. With the development of aerospace science, especially the appearance of high speed attack weapons such as guided missile, radar is required to not only discover and track the target in further distance but also command plane and missile to head off the target

    隨著空間技術的發展,特別是等高速武器的出現,要求雷達能在更遠的距離上發現和跟蹤目標,並能及時指揮和引飛機和攔擊目標。
  3. Recently, much attention has been paid to the thin films of tunable dielectric materials for their applications in microwave agile devices, such as phase shifters, tunable filters, and voltage - controlled oscillators ( vcos )

    隨著等快速武器的發展,對雷達的功能提出了許多新的要求。採用機械掃描方式的天線已很難適應新的作戰要求。
  4. Fourthly, we discuss and simulate the transformation method of relative parameters of ground target based on data link. and then we analyze decision algorithm of air - to - ground attack. especially, we educe three dimensional terminal guidance law of air - to - ground missile in the disturbance of wind, and give the simulation result

    本文也研究了空對地擊的若干技術,包括對獲得數據鏈指揮下地面目標相對于某擊機當前時刻相關參數的方法行了闡述及模擬,並在此基礎上討論了單機對地面多個目標的擊決策演算法,同時提出了一種風干擾下空地的三維末制引律,且利用數字模擬行了驗證,並指出研究空地引律時考慮風影響的必要
  5. 5. improve and simplify the original algorithm for missile attack range, making the calculation faster and more efficient

    擊區的計算方法及類比例引法,提高了計算速度,改善了實時
  6. Within the past week, unmistakable evidence has established the fact that a series of offensive missile sites is now in preparation on that imprisoned island

    在上周,有清晰的證據顯示了這樣的事實? ?在那個被囚禁的小島上一系列進攻性導彈場地正處在建設中。
  7. In october he began to talk about offensive missile bases.

    十月間,他開始談到基地了。
  8. In this paper, firstly, three - dimensional geometrical models of the target and ir flares are established and by using the software vega missile attacking process is real - time simulated visually. secondly, the ir radiation characteristic of the target, background and the ir flares are analyzed, in which the wave radiation of the sun at different time, wind speed, the relative humidity and ir radiation attenuation characteristic of the atmosphere is under consideration. from above the ir image of the target, ir flare and the background are got and then are normalized to gray color image that will be showed in a child window in real time

    本文通過三維建模工具creator建立目標、背景和干擾的三維模型,再通過視景模擬軟體vega生成載機、和目標飛機的可見光場景圖像,實時地對擊工程行可視化模擬;並分析了目標、背景和干擾的紅外輻射特,計算出傳感器路徑上大氣衰減等等,將經過衰減的目標、背景和干擾的輻射強度量化為灰度圖,以子窗口形式實時顯示;一步可以使目標和干擾按照各自的運動軌跡運動,便可產生動態的紅外熱圖像序列。
  9. Forth, this thesis also had made a preliminary discussion on the integrated guidance system of air - to - air missile beyond visual range air combat and made deep research on the midcourse guidance stage, thus we obtained an extremely useful conclusion.

    本文還對空空超視距擊的復合制體製做了一個初步的探討,並對其中的中制階段行了深入研究,得到了一個十分有用的結論:即中制階段發動機的最優推力方向實際上應該是關于時間的線函數。
  10. China s extensive and well - established ballistic missile industrial infrastructure continues to concentrate on replacing liquid - propellant missiles with mobile solidpropellant ones, reflecting concerns for survivability, maintenance, and reliability and developing high - priority lacms for theater and strategic missions

    中國龐大而全面的工業基礎設施繼續側重以移動固體推取代液體推,並重視的持久、維護及可靠,同時作為重點項目積極研製用於戰區和戰略使命的陸巡航
  11. 6. utilizing the new robust decoupling control method which is put forward above, the design problem of decoupling controller for large angle of attack reentry missile ' s attitude control system is mainly investigated

    6 、針對大角再入飛行通道間存在的氣動耦合現象,以及實際飛行中存在的個確定因素,分析了其行解耦控制的必要;探討了本文提出的基於互補靈敏度成形和h 。
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