飛機機動飛行 的英文怎麼說

中文拼音 [fēijījīdòngfēiháng]
飛機機動飛行 英文
aircraft maneuver
  • 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...
  • 機 : machineengine
  • 行 : 行Ⅰ名詞1 （行列） line; row 2 （排行） seniority among brothers and sisters:你行幾? 我行三。where...
  • 飛機 : airplane; plane; aeroplane; kite; bird; aircraft
  • 機動 : 1 （利用機器開動的） motor driven; motorized2 （權宜; 靈活） flexible; expedient; mobile; manoeuv...
  • 飛行 : flight; flying; aviate; voyage; volitate; hop
  1. The probe - and - drogue method also placed a high workload on the pilot of the receiving aircraft because the early drogues were not very stable and tended to wander in tight circles

    探頭錐管的方法對于受油機的飛行員來說是一項很高的工作負擔，因為早期的錐管並不十分穩定而是在一個小的圓圈裡擺動。
  2. Many factors were considered in the algorithm such as the helicopter nonlinear flight dynamic model, the time delay of rotor wake, the air compressibility at advancing blade, the stall of retreating blade, the unsteady flapping motion of rotor blades and the aerodynamic interaction among rotor, fuselage, tail rotor and empennage

    根據這一方法可以確定為完成直升機機動飛行所需的駕駛員操縱輸入及直升機的飛行速度、角速度和飛行姿態的變化歷程。
  3. On the basis of introducing the principle of the tf / ar radar, this paper analyzes the conditions of effectively jamming the tf / ar radar in typical tactical act of hedgehopping, which include the disposition and quantity of electron reconnaissance / jammer, calculates the capability request of equipments in the method of sensor / hand - emplaced jammer, and concludes that it is difficult to jam tf / ar radar at the present time

    摘要在介紹地形跟隨迴避雷達工作原理的基礎上，通過設定典型超低空突防飛機的戰術行動，分析了對雷達實施有效干擾所必須具備的條件，包括偵察干擾機的部署、數量要求等；並計算了在傳感器擺放（投擲）式干擾機模式下對裝備的性能要求，得出了在目前技術條件下，對地形跟隨迴避雷達實施干擾在技術和戰術上都是困難的。
  4. A sonic boom is the loud crash and shaking that happens when a jet plane goes faster than the speed of sound

    聲爆是當噴氣式飛機超音速行駛時產生的巨大碰撞和搖動聲。
  5. The paper applyed principle analysis and numerical computation to compare the scheme of particle injection syphon and convergence - turn tube. the last method was adopted to conduct research because it could produce high concentrated particles stream and operated conveniently. 2

    本文應用原理分析、數值計算等手段，對粒子加入、彎管和收斂?折管方案進行了比較，認為收斂?折管方案可以產生發動機在飛行過載中的凝相粒子聚集效應，且燒蝕參數控制方便。
  6. For validating the feasibility, generality, and validity of the laboratory design scheme, chapter 3 presents a demonstration model, which uses the fuel system of an aeromodelling as the research object

    為了驗證本方案的可行性、通用性和先進性，在第三章利用航模飛機發動機燃油系統作為研究對象，給出了一個演示驗證系統。
  7. In addition, a series of reasonable time histories of helicopter velocity, angular velocity and flight attitude were shown during the given dolphin maneuver flight

    最後以黑鷹直升機為例計算了魚躍越障機動飛行時駕駛員操縱輸入及直升機速度、角速度和飛行姿態的變化規律。
  8. As opposed to the usual practice of pilot reporting the weather to the air traffic controller, this time the equipment on - board the aircraft did the job for him

    當日一班國泰航空公司的班機飛離香港，期間飛機自動進行十次天氣觀測，並將觀測報告傳回本港。
  9. Fuzzy neural network control with application to post - stall maneuvers

    模糊神經網路在過失速機動飛行中的應用
  10. At the end, the vibration responses are displayed in polar diagram synthetically, in which the displacement, the static offset and the deflection angle of rotor could be shown altogether

    提出用極坐標表徵轉子振動特性的方法，可以更直觀、全面地反映轉子的振動幅度、機動飛行時的靜態偏移以及偏擺角。
  11. The thesis describes the conception of the object - oriented modeling and integrated simulaton enviroment, and discusses the below topics : ( 1 ) describe the reasonable structure of the modern fighter simulation system, and design the data transfer interface. ( 2 ) discuss the modeling method of the key subsystem of future fighter system especially the aerodynamics and the control system in detail. ( 3 ) construct the 3d model of the aircraft and scene, and verify the graphic simulation technique based on pc

    本文詳細討論了面向對象建模方法以及一體化模擬環境的基本概念框架及基本結構並在此基礎上提出了合理的現代戰斗機模擬系統結構，設計了模擬系統的數據傳遞介面；詳細討論了現代戰斗機模擬系統關鍵子系統? ?飛機本體、飛行控制系統建模方法；建立了用於研究的飛機以及視景的三維顯示平臺；並在此基礎上實現了實驗性的基於pc的現代戰斗機圖形模擬平臺，對模擬模型有效性確認和驗證工作做了初步的探討，研究比較了傳統飛行動力學和運動學方程和四元數法在飛行模擬中的效果。
  12. Modern high - performance fighter planes can develop very high acceleration ( + gz ). under such a situation, pilots have to undertake a high - sustained g acceleration stress, which may produce loss of consciousness ( g - loc ), even result in fatal flight accidents

    現代高性能戰斗機在機動飛行中可產生很高的正加速度（ + gz ） ，飛行員中+ gz致意識喪失（ g - loc ）的發生率增多，對飛行安全構成嚴重威脅。
  13. Abstract : this paper presents an inverse simulation algorithm of determining the pilot control law as well as the time histories of helicopter velocity, angular velocity and flight altitudes to follow a given helicopter maneuver flight path

    文摘:本文給出了一種直升機機動飛行的逆模擬方法以計算跟隨預定飛行軌跡的駕駛員操縱。
  14. Under the requirement of multi - maneuver flight mission, spacecraft sometimes has to perform autonomous navigation by using on - board sensors in a short time

    未來多任務航天器往往要執行多次機動飛行，由於地面導航的局限性，需要在較短的時間內對航天器進行自主導航。
  15. On the sensitivity of aircraft longitudinal flying qualities to aerodynamic derivatives at high angle of attack

    飛機縱向飛行品質對大迎角氣動導數的敏感性研究
  16. First of all, it is devoted to discuss the open - loop characteristics and the nonlinear bifurcation analysis and the maneuver ability for the super - maneuverable flight nonlinear model of the new generation fighter. then a flight control system is designed in analytical dynamical inversion method based on the time - scale separation principle

    首先，對新一代殲擊機超機動飛行的非線性模型的開環特性、分叉特性及機動能力進行分析，並以此模型為基礎，採用基於時標分離原則的動態逆控制方法設計了新一代殲擊機的飛行控制系統。
  17. Then s - style high maneuver trajectory with high angles of attack is simulated by given control commands of angle of pitch

    進行了俯仰平面s型軌跡機動飛行模擬，模擬結果說明了大攻角飛行的高機動特性。
  18. Image movement that is brought by aeroplane movement ( including the forward movement, pitching and yawing movement ) will be eliminated, and then image quality of camera will be improved after the research

    通過本文的研究，消除機載平臺產生的像移（指飛機前向飛行和俯仰偏航運動引起的像移誤差） ，提高相機成像質量。
  19. Simulation that is the developing of the flight dynamics of helicopter is the best way to study maneuver flight of helicopter

    計算機模擬是研究直升機機動飛行最有力的手段，直升機模擬技術也是直升機飛行動力學發展的方向之一。
  20. Then several typical maneuvers are picked up to simulate, and the result shows that the control system can satisfy the design specification of ads33d criteria

    並且選取幾個典型的機動飛行科目進行模擬，結果表明達到ads33d標準要求。
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