控制導彈 的英文怎麼說

中文拼音 [kòngzhìdǎodàn]
控制導彈 英文
direct a missile
  • 控 : 動詞1 （告發;控告） accuse; charge 2 （控制） control; dominate 3 （使容器口兒朝下 讓裏面的液體慢...
  • 制 : Ⅰ動詞1 （製造） make; manufacture 2 （擬訂; 規定） draw up; establish 3 （用強力約束; 限定; 管束...
  • 導 : 動詞1. （引導） lead; guide 2. （傳導） transmit; conduct 3. （開導） instruct; teach; give guidance to
  • 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
  • 控制 : control; dominate; regulate; govern; manage; check; cybernate; manipulate; encraty; rule; rein; c...
  • 導彈 : guided missile
  1. For quick truning to target of air - to - air missile ( aam ) for short range dogfight in large off - boresight it is necessary to study the agile turn control law

    摘要為了使近距格鬥空空導彈在大離軸角發射時能快速地轉向目標，需要研究快速轉彎控制律。
  2. Segment sliding mode control of missile ' s electromechanical actuation

    導彈電動舵機系統的分段滑模控制
  3. So the recent introduction of the microcomputer has provided a further impetus towards the possibility of on-line optimisation, or true adaptive control, within the missile itself.

    最近微型計算機的出現，一定會促進聯機最佳化，或者導彈內部的真正的適應控制的可能性。
  4. This paper integrates direct lateral force control with aerodynamic control, taking the anti - aircraft missile which has the anti - guided ability in the aerosphere as research subject

    本文的研究對象為大氣層內具有反導能力的防空導彈。主要研究內容為把直接側向力控制與氣動力控制結合。
  5. Abstract : the paper emphasizes on exoatmospheric antimissile missile rapid reaiming problem, and according to pontryagin ' s maximum principle the optimal control law in the conditions of long miss distance and long elimination time is presented

    文摘:針對大氣層外反導導彈快速重新瞄準問題，在脫靶量和消除它的時間都比較大的情況下，用龐特里亞金極大值原理求出了最優控制規律。
  6. Identical autopilots are used to control the pitch and yaw motions if the missile has two planes of symmetry.

    如果導彈有兩個對稱面，則使用相同的自動駕駛儀控制俯仰和偏航運動。
  7. In order to design the autopilot for a rear controlled missile we must make a first estimate of the required aerodynamic derivatives.

    為了設計尾部控制導彈的自動駕駛儀，我們必須首先估算一下所需要的氣動力導數。
  8. In contrast to the aerodynamic winged vehicle, a true ballistic missile is controlled for only a few minutes at the start of its flight.

    與空氣動力有翼導彈大不相同，一枚真正的彈道導彈只在起飛的幾分鐘內受人們控制。
  9. 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。
  10. Evaluation of the operational effectiveness of stand - off air - to - ground television remote control missile

    防區外空地電視遙控制導導彈作戰效能評估
  11. Design of missile vertlcal lanch system based on sing - chip control

    基於單片機控制導彈垂直發射系統設計
  12. Earths future on your bodies. game, around key control chariot and move around th

    游戲方法，左右方向鍵控制戰車左右移動，鼠標控制導彈發射的方向。
  13. The task of the missile control system is to guide the missile to the object, then smash it

    導彈控制系統的設計任務就是實現對導彈的控制，控制導彈飛向目標，最後擊毀目標。
  14. And the traditional designed autopilot has poor robustness, so it should shift the autopilot ' s gain for the btt missile flying stably along the whole trajectory

    又由於用傳統方法設計的自動駕駛儀魯棒性不高，為控制導彈沿全彈道飛行，需逐段切換自動駕駛儀的增益。
  15. This thesis uses fuzzy changing the gain proportion guidance to control the yaw angle v and the pitching angle, and to realize following track, with the predetermined track, which had been designed by hierarchical track planning with voronoi diagram

    本文在利用voronoi圖的分層航跡規劃，規劃出預定航跡，並利用模糊變增益比例制導律控制導彈的偏角v和彈道的傾角，實現航跡跟蹤。
  16. Operation effectiveness evaluation of television guided missiles

    電視遙控制導導彈的作戰效能評估
  17. Simulation and evaluation of the combat effectiveness of television remote control missile

    電視遙控制導導彈作戰效能評估與模擬
  18. Simulation of combat effectiveness for tv telecontrol guided missile in complex background environment

    復雜環境空地電視遙控制導導彈作戰效能模擬
  19. Mixed weights cgpc is constructed for constrained cgpc, which has advantage in simplicity and efficiency. performance of ballistic missile ’ s servo system is improved by approximate constrained arithmetic. the effect of side force on stability of spinning missiles is studied by routh criterion, which proved to be more universal than others ’ work

    針對線性角運動模型，直接採用勞斯方法，與前人工作相比具有更好的通用性和精確性;藉此方法近似分析了側向力對自旋彈道導彈穩定性的影響;研究了內模控制在彈道導彈姿態穩定系統中的應用。
  20. Sliding mode control based on nbf net to integrated guidance autopilot design for missiles

    網路的導彈航向平面滑模控制導引一體化
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