small missile 中文意思是什麼

small missile 解釋
小型導彈
  • small : adj 1 小 (opp large) 少 (opp large numerous) 細小的;窄小的;瑣細的;些微的;少額的(收入等)...
  • 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. A small mobile missile can help make america's land-based arsenal more secure.

    小型機動式導彈會有助於使美國的陸基武庫轉為安全。
  2. Cruise missile with many good qualities, such as wide uses, high precision, big power, small volume, doughty charge ability, speedy corresponsive ability, high function - cost proportion. because of the good qualities had by ballistic missile and plane, the cruise missile is a lethal weapon that constitute a weighty threat to enemy states in the modem war

    巡航導彈具有用途廣、精度高、威力大、體積小、突防能力強、反應速度快、效費比高等特點,正是由於巡航導彈兼有彈道導彈和飛機的諸多優長,所以它便成了現代戰爭的「殺手鐧」 ,成為對敵方構成重大威脅的重要武器。
  3. New method of small sample experiment for the simulation system with hardware in the loop for homing missile

    新的尋的導彈半實物模擬系統小樣本實驗方法
  4. Both advantages of rocket engine and air - breathing engine are integrated into one kind of propulsion system, called rocket - based - combined - cycle ( rbcc ), which has multiple operating woke modes, including ejecting, subsonic combustion, supersonic combustion and rocket mode, with each mode operating at varying flying stage. rbcc has prominent potential of high efficiency and low cost, and so it is recognized as an advanced propulsion system of future single - stage - to - orbit reusable spacecraft and hipper - sonic missile. it has been broadly investigated in foreign countries and has been progressed into small and full - scale flying stage

    火箭基組合動力循環( rbcc , rocketbasedcombinedcycle )將傳統的火箭發動機和吸氣式發動機的優點集中組合到一個具有多種工作模態(包括引射、亞燃、超燃及火箭模態)的發動機里,在不同的飛行階段啟用不同的工作模態,因此具有大幅提高航天推進系統經濟性與高效性的潛在優勢,並可能發展成為下一代單級可重復使用航天器以及高超聲速導彈武器的動力系統。
  5. It has the characteristic of non - gear - box, large output torque, small volume, easy control, fast response, high track precision, high reliability etc. the system has potential advantages over substituting for traditional hydraulic or pneumatic missile actuator servo control system and has wide prospect in the fields of aerial actuator, servo valve, robot, radar antenna etc. the system ' s operation principle, control idea, functions and realization of each component are discussed in detail

    該系統在取代傳統的液壓、氣動導彈舵機伺服控制系統方面有很大潛力,同時在航空舵機、伺服閥,以及機器人關節的直接驅動、雷達天線等領域具有廣闊的應用前景。論文詳述了系統的工作原理與控制思想,以及系統方案的設計和各組成部分的功能與實現方法。
  6. The big problem is to make a laser small enough ! to fit in a satellite, yet power nil enough to destroy a missile at a range of 2, 000 kilometers

    關鍵是要製造一種激光裝置,讓它小到能夠衛星,威力又要強到足以摧毀2000公里射程內的導彈。
  7. There was a whiz as of a missile in the air, mingled with the murmur of a curse, a sound as of shivering glass followed, and a small, vague form went over the fence and shot away in the gloom

    隨后,只見有個什麼東西混雜著一聲輕輕的咒罵聲,嗖地一聲在空中劃過,接下來就聽到一陣打碎玻璃的聲音,之後,就見一個小小的模糊的人影翻過柵欄,在朦朧的夜色中箭一般地飛跑了。
  8. The prerequisites for a nation, or a nonstate entity, to conduct a hane are relatively straightforward : a small nuclear weapon and a standard ballistic - missile system, something not much more sophisticated than a scud

    一個國家或非國家實體要進行高空核爆,先決條件其實相當簡單,只要擁有小型核子武器和標準的彈道飛彈系統,而這類系統並不比飛毛腿導彈( scud )復雜。
  9. The direct lateral force control is that more than one hundred small jet engines are installed around the missile before the barycenter. by firing up these engines produce impulse propelling force in order to adjust the position of the missile

    姿控直接力控制方式是在導彈四周重心前徑向安裝的很多個小型噴流發動機,控制噴流發動機點火,產生脈沖推力,對導彈進行姿態調整。
  10. The jellyfish floating face a big crisis, zhang your mouth and forward it to operate guide : space, the key to control movement, a missile launch capability, s eat too much plankton d. ordinary small attack

    浮遊的水母遇到了大危機, ,張大你的口向前沖吧操作指南:空格開始,方向鍵控制移動, a發射能力彈, s張大口吃掉小浮游生物d普通攻擊
  11. Introduction : the jellyfish floating face a big crisis, zhang your mouth and forward it to operate guide : space, the key to control movement, a missile launch capability, s eat too much plankton d. ordinary small attack

    攻略:浮遊的水母遇到了大危機, ,張大你的口向前沖吧操作指南:空格開始,方向鍵控制移動, a發射能力彈, s張大口吃掉小浮游生物d普通攻擊
  12. The gliders suck in and shoot out water to change their buoyancy and move up and down. small wings on their missile - like bodies create lift to move horizontally. without a noisy propeller or engine, the gliders run silently and on very little power

    這種水下滑翔機長6英尺1 . 83米重100磅45 . 4公斤,依靠吸進吐出海水改變浮力,並藉助側翼產生水平動力。
  13. Combination algorithm fully use the advantage of the ukf for small noise and the upf ’ s non - sensitivity to noise, when noise increase, upf can also estimate the missile ’ s states well

    聯合演算法充分利用了ukf在噪聲較小時估計效果較好和upf對噪聲不敏感的特性,使得當觀測噪聲突然增大后,利用upf演算法仍能使導彈位置和速度誤差收斂,達到有效預警的目的。
  14. Based on the small tactical missile system design, an engineering method for ram - air servo system dynamic accuracy analysis and verifying unit design is put forward

    摘要從小型戰術導彈總體設計的角度提出了一種繼電控制沖壓式伺服系統的動態精度和校正裝置的工程分析和設計方法。
  15. All of above make the miss distance of the missile difficult to estimate in shooting range. in order to solve these problems, a novel method for detecting and tracking small moving point target in image sequence is proposed in this paper, based on combination of the correlation of multi - frames and wave gate techniques. especially, the qualifications to confirm the target and the establishment of the wave gate based on size and characteristic moving parameters of the target are stressed in the paper

    針對目前靶場所面臨的測量目標小、距離遠、目標與背景對比度小,不具有形狀信息的實際問題,提出了一種基於多幀相關技術與波門選通技術相結合的快速目標識別與跟蹤方法,特別探討了多幀相關技術中目標確定的理論判據,並綜合考慮目標的尺寸因素和目標的運動特徵研究了一種新的波門設定方案。
  16. New trend in development of us military space technology is overviewed, such as us air force four space mission areas which include space force enhancement, space force apllication, space support and space counter, operationally responsive space ( ors ), new space millitary carrying vehicles, small military satellites and advanced missile defense technology also discribeted

    摘要綜述了美國在軍事空間技術新的發展動向,包括美國空軍的「空間軍力加強、空間軍力應用、空間支授、空間對抗」四大空間軍事任務區,快速響應空間,新的空天進攻飛行器,軍事小衛星運載器,軍事小衛星,導彈防禦先進技術等的發展動態。
  17. As for conventional weapons, it ’ s low cost, easy to maintain, flexible to use and consumed heavily ; especially when there are multi small targets, cannon shell could be superior to missile in damaging effect, so many countries make precision guided munitions as the primary developing direction of the conventional arms

    常規武器制導造價低、易於維護、使用靈活、消耗量大,尤其是在面對多個小型目標時,制導炮彈的打擊效果要比導彈好許多,因此,很多國家都明確地把精確制導武器列為常規武器發展的重點;相比之下,我國在這方面的發展則顯得比較落後。
  18. 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
  19. 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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