攔截飛彈 的英文怎麼說

中文拼音 [lánjiéfēidàn]
攔截飛彈 英文
antiballistic missile
  • 攔 : 動詞（不讓通過; 阻擋） bar; block; hinder; obstruct; hold back
  • 飛 : Ⅰ動詞1 （鳥、蟲等在空中活動） fly; flit 2 （利用動力機械在空中行動） fly 3 （在空中飄浮遊動） fly...
  • 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
  • 攔截 : intercept
  • 飛彈 : 1 （有自動飛行設備的炸彈） missile; missile plane; fly bomb; doodlebug; flying bomb; buzz bomb2 ...
  1. Ironically, use of an antimissile interceptor against a nuclear - tipped target with a proximity fuse could in fact set off a destructive hane phenomenon

    諷刺的是，如果使用反飛彈攔截裝置對付具備近炸引信的核彈頭目標，反而更容易造成破壞性的高空核爆現象。
  2. So unless the pentagon is prepared to carpet the nation with interceptors, it is clear that terminal defense is not an appropriate response to the threat of a few nuclear - armed icbms

    所以，除非五角大廈準備在美國各地全面部署攔截器，否則終端防禦系統並不適合用來因應核子洲際彈道飛彈所造成的威脅。
  3. Spinning flight of ballistic missile in boost phase is a new idea in order to penetrate laser ’ s interception. spinning missiles may be unstable due to dynamic and control interactions

    彈道導彈主動段自旋飛行是一種新的構想，旨在對抗激光武器攔截，實現主動段突防。
  4. This design method overcomes the traditional autopilot ' s disadvantage that should shift the autopilot ' s gain according to flight phase ; it also can make the btt missile fly stably along the whole trajectory, and can intercept a maneuvering target accurately

    該設計方法克服了傳統自動駕駛儀在控制導彈飛行中需逐段切換增益的不足，能控制btt導彈在大空域內沿全彈道穩定飛行，並能精確攔截機動目標。
  5. The ground - based midcourse defense system, as it is called, will start off with no more than 10 “ hit - to - kill ” interceptors designed to collide directly with incoming missiles in space

    在初期，陸基中層防禦系統只有10枚以下的擊殺攔截載具，設計用來在太空直接撞擊並摧毀來襲飛彈。
  6. To solve the problems caused by the varieties of the missile dynamics with the difference of flight height, velocity and attitude angle in modeling the missile, in this thesis, the theory of variable structure model reference adaptive control is used to design a pitch channel autopilot based on a longitudinal missile model, the status equation using the measurable parameters of load and angular rate is established, and the methodology to choosing the reference model is discussed also, and the performance of the controller is analyzed by means of simulation

    為了解決攔截彈氣動參數隨飛行高度、速度、姿態的不同，變化范圍大，控制系統難以準確建模的困難，基於縱向平面攔截彈模型，採用模型參考變結構控制理論設計了俯仰通道姿控復合控制系統，以可測量變量過載和角速度作為狀態量建立了系統的狀態方程，討論了參考模型的選擇方法，並對系統的性能作了模擬分析。
  7. This group focus on the research of missile and launch vehicle, which contain the guidance law and the controller design. there are two researchers in this group now, including one m. d

    本研究群的宗旨乃進行攔截飛彈及運載火箭之研究，主要包含導引法則及自動駕駛儀控制器設計等項目，並利用各式各樣的模擬（其中也包含空氣動力學模型） ，驗證其系統可行性。
  8. The simulation results show that the btt missile ' s robust autopilot designed on a standard state point can make the btt missile fly stably along the whole trajectory, and has the ability of intercepting maneuvering targets

    模擬結果表明：本文按給定空域內一個特徵點設計的btt導彈魯棒自動駕駛儀能控制btt導彈在該空域內沿全彈道穩定飛行，並具有攔截機動目標的性能。
  9. To date, the program has intercepted target missiles in five of eight heavily scripted tests

    到目前為止，這項計畫已在八次作秀性質的測試中，五次成功攔截到目標飛彈。
  10. With the new generation missiles / interceptors entering a period of rapid development, guidance by seeker is one of key technologies for these weapons, but the complicated disturbance caused by high speed missiles / interceptors traveling through the atmosphere will degrade the tracking & aiming sensor system of the seekers, even worse, will make the guidance system fail to function

    為了在現代高技術局部戰爭取得優勢， 「遠程打擊與保護」已被提到一個相當重要的地位，新一代導彈和攔截武器進入了日新月異的發展時期，制導技術是這類武器的關鍵技術之一。而高速飛行的導彈周圍會產生很復雜的氣流擾動，這種擾動對導引頭上的跟瞄系統將產生很大的影響，嚴重時可造成導彈制導系統完全失效。
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