攔截彈道 的英文怎麼說

中文拼音 [lánjiédàndào]
攔截彈道 英文
intercept trajectory
  • 攔 : 動詞（不讓通過; 阻擋） bar; block; hinder; obstruct; hold back
  • 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） ...
  • 攔截 : intercept
  1. 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。
  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. Exoatmospheric kinetic interception is an important resort of ballistic missile defense. thus the research and study on exoatmospheric kinetic vehicle is significant for the technological improvement of national ballistic missile defense

    大氣層外動能攔截是彈道導彈防禦的重要手段，因此對大氣層外動能攔截器的跟蹤研究對我國彈道導彈防禦技術的發展有重要意義。
  5. 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。
  6. 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。
  7. First, proper initial conditions between ekv and target are the premise of hit - to - kill. capture region is described by equations of relative motion defined in modified polar coordinate while phasetrajectory graph is introduced. and the disturbance of initial condition biase is analyzed by cadet through statistical linearization of ekv dynamical model

    本文在修正極點坐標系中建立攔截器和目標之間的相對運動方程，結合相平面軌跡圖，分析了大氣層外動能攔截器的攔截區;對大氣層外動能攔截器動力學模型進行統計線性化，採用協方差分析描述函數法，分析了初始狀態誤差對彈道的影響。
  8. The two countries signed an agreement in june to work together on an advanced ballistic missile defense shield, using interceptor missiles to shoot down enemy rockets

    美日兩國6月簽署協定，共同研製一套先進的彈道導彈防禦系統，使用攔截導彈擊落敵方火箭。
  9. Miss distance simulation for kinetic kill vehicle intercepting tactical ballistic missile

    動能攔截器攔截戰術彈道導彈的脫靶量模擬
  10. 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。
  11. The high - altitude, long - endurance ( hale ) unmanned aerial vehicles ( uav ) is used to carry out high reconnaissance or to head off missiles

    高空長航時無人機主要執行戰略偵察監視任務，也可用於空中預警、通訊中繼、電子干擾、戰區彈道導彈的攔截。
  12. 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。
  13. Abstract : in order to achieve effective breaking through the enemy s anti - missile defense theatre and avoid intercepted by anti - missile defense system, many breakthrough methods have been implemented in middle course and re - entry phase of ballistic missile to protect the missile from acquisition, tracking and recognition by anti - missile system

    文摘:彈道導彈為實現有效的突破反導防區而不被防禦系統攔截，在其彈道中段和再入段採用了多種突防措施，以免受反導系統的搜索、跟蹤和識別。
  14. 4. the simulations of btt missile against maneuvering targets are studied

    對btt導彈攔截機動目標進行了全彈道模擬。
  15. X - band ground based radar ( gbr ) plays an important role in national missile defense ( nmd ) system, it has many important functions such as middle stage surveillance and interception, trajectory prediction, target identifying and classifying. it has important significance to analyze and study gbr system, not only for ballistic missile ’ attack and defense research, but also for our national space surveillance and ballistic missile defense system development

    X波段地基雷達（ gbr ）是美國國家導彈防禦系統中段防禦和攔截系統中最主要和最有效的目標精確跟蹤和識別傳感器之一，它負責中段監視和截獲、預測彈道和實測彈道的精度、識別和目標分類等重要功能，對gbr的系統分析和模擬研究，探究其工作機理和識別手段，不但對于研究彈道導彈的有效突防措施和攻防對抗有著重要意義，對于發展我國自己的空間監測和彈道導彈防禦系統也有著重要的參考價值。
  16. Multitarget interception is a big difficult problem in ballistic missile defense, and is also the most arduous technology of the missile defense system of us

    摘要多目標攔截是彈道導彈防禦的重大難題，也是目前美國導彈防禦系統所遇到的最大的技術難點。
  17. The main works of this thesis are research of lateral force control and guidance of interceptors, emphasized on the terminal phase when intercepting the tactical ballistic missiles, including the performance analysis of extra - atmospheric kinetic - kill vehicle piloted by trajectory - control and attitude - control systems, and combined control of aerodynamics with lateral jets in atmosphere

    本文主要研究攔截彈在攔截戰術彈道導彈時，末段的制導和側向力控制問題，包括大氣層外動能攔截器在姿控與軌控發動機作用下的性能分析，和大氣層內側向力與氣動力復合控制研究。
  18. The results show that the performance of the combined control system designed in this thesis was superior to the traditional only aerodynamic control system, and the warhead of tactical ballistic missile with medium velocity could be intercepted

    結果表明，所設計的復合控制系統較純氣動力控制系統性能有所提高，能夠攔截中等載入速的戰術彈道導彈。
  19. 5. aiming at the specific mission that intercept the warhead of tactical ballistic missile, the new issue for designing the guidance law is analyzed, and a new guidance method that fit for the mid - course is presented, based on the idea of predicting the intercept point. to design a feasible terminal guidance law, the shortcoming existing in the proportional navigation when intercepting the warhead is firstly

    針對攔截戰術彈道導彈這一特殊任務，分析了導引律設計面臨的新問題，提出了以預測攔截命中點為思想的中制導段導引方法，研究了末制導段比例導引律彈道形狀和過載分佈特點，在此基礎上為了改善比例導引律的缺陷，引入了目摘『要標機動加速度和導彈軸向加速度等信息、 ，又寸比例導引律進行了修正，井對導引律中各參數進行了優化。
  20. Study on the model of intercepting decision for multi channel surface to air missile weapon system

    多通道地空導彈武器系統攔截決策模型研究
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