飛機的操縱 的英文怎麼說

中文拼音 [fēijīdecāozōng]
飛機的操縱 英文
aircraft control
  • 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
  • 的 : 4次方是 The fourth power of 2 is direction
  • 操 : Ⅰ動詞1 （抓在手裡; 拿; 掌握） hold; grasp 2 （做; 從事） act; do; operate 3 （用某種語言、方言說...
  • 縱 : Ⅰ動詞1 （釋放; 放走） release; set free; let go 2 （放任; 不約束） indulge; give oneself up to; l...
  • 飛機 : airplane; plane; aeroplane; kite; bird; aircraft
  • 操縱 : 1. （控制; 開動） operate; control; roll; steer 2. （支配;控制） rig; manipulate; govern
  1. The control stick of an aircraft

    操縱桿飛機的操縱桿
  2. Several icing parameters were imported to calculate the change of drag coefficient and typical derivatives between clean aircraft and iced aircraft, and the aircraft flight envelope change of iced and un - iced situation was computed, and the small disturbance flight dynamics model was modified to study the effect of the ice accretion on the aircraft dynamics by importing the ice parameter to it, and the longitudinal and lateral stability and the elevator, aileron and rudder step response were also studied and simulated

    根據這些參數計算了飛機結冰后阻力系數以及典型氣動導數的變化，並計算了結冰前後飛機的飛行包線；同時對結冰前後飛機的縱向、橫側動穩定性以及升降舵、副翼和方向舵階躍操縱響應進行模擬計算。
  3. The airplane ' s handling qualities continue to be very good throughout the flight envelope

    在整個飛行包線內這架飛機的操縱品質也是相當的出色。
  4. These advantage make it excellent materials for control surface, wing and skin of airplane

    是飛機結構中對剛度要求較高的操縱面、機翼和機身蒙皮結構用較理想的材料。
  5. This perfect control made their sliding safe and allowed them to proceed to the powered airplane.

    這種完善的操縱機構，使他們能安全滑翔並進一步製造有動力裝置的飛機。
  6. He manipulated the controls of the plane so well that it did not crash

    他將飛機的操縱裝置操縱得多麼熟練以使它沒有撞機。
  7. The players task is to control the center of the screen iaf aircraft, floated around the meteorite shooting, after their crushing the white diamonds collected. the next key counterparts around the aircraft directional movement, forward, back, left to the left, right to the right, pressing the space bar to the fire, can fire bullets as long as the shooting gray meteorites white diamonds will be there, it needs attention, not e

    方向鍵上下左右對應飛機的四向移動， 「上」為前進， 「下」為後退， 「左」為左轉， 「右」為右轉，按下空格鍵為開火，子彈可以連發，只要射中灰色的隕石，就會有白色鉆石出現，需要注意的是，並非每顆隕石擊碎都會出現鉆石，有時還會夾雜著一些碎片，玩家需要操縱飛機躲開碎片，否則會扣去飛機的能量槽。
  8. The approach maintains the simplicity of the original algorithm, and carry out perfect model following. the pseudo - inverse method is concerned with distributing the deflection commands of multiple control surfaces of the aircraft to generate required control responses when the number of independent control surfaces is greater than the number of required independent control responses

    偽逆演算法通過改變反饋增益來實現故障系統的控制律重構，當一個操縱面發生故障后，可改變控制律重新分配控制指令，利用其它操縱面來實現它的功能，近代先進飛機多採用此方法來提高飛機的容錯能力。
  9. During aircraft take - off and landing phases, the dynamic loads and vibrations caused by landing impact and the unevenness of runway will result in airframe fatigue, discomfort of passenger and the reduction of the pilot ' s ability to control the aircraft

    在飛機起飛和著陸過程中，由著陸沖擊和跑道不平引起的沖擊載荷和振動，會造成飛機機體疲勞損傷、乘客不適及地面駕駛操縱能力的降低。因此，在設計飛機起落架緩沖器時，必須限制起落架傳遞給飛機的沖擊載荷。
  10. The results show that there are no un - receptible responses when the post stall maneuver modes are applied, and agility is raised significantly

    試驗結果表明，使用的4種過失速機動控制模式沒有不可接受的操縱響應，飛機採用推力矢量控制后敏捷性明顯提高。
  11. He sat at the controls of the aircraft

    他坐在飛機的操縱裝置前。
  12. The design of aircraft cockpit, which acts as the man - machine interactive interface is of great research value. the author utilizing advanced cad technology, combining the intersecting knowledge with man - machine engineering, robotics, aero - human - engineering, etc, has exploited corresponding modules, such as the simulation of pilot manipulation, vision checkout, vision simulation, accessibility calculation, manipulation force calculation, and established a set of subsystem of aircraft - cockpit - design on the platform of catia

    本文利用先進的計算機輔助設計（ cad ）手段，結合人機工程學、機器人學、航空人體工程學等邊緣交叉學科知識，在catia平臺上，利用其二次開發語言vbscript ，實現了相應的飛行員操縱動作模擬、視界檢查、視覺模擬、可達性計算和操縱力計算等功能，初步建立起一套飛機座艙設計cad子系統。
  13. The superposition between the helicopter rotor induced flow and the warship airwake leads to the formation of the complex wake, which affects the helicopter ' s control response and flight safety during take - off and landing from a warship

    摘要直升機旋翼誘導流與艦船空氣尾流疊加后形成復合流場，對直升機艦上起降時的操縱響應及飛行安全有很大的影響。
  14. If electric actuators is used for power souce of the controling braking and hydraulic pressure of the plane, the system of hydraulic pressure woulde be cancelled or reduced. then the reliability and maintain woulde be increased and the weight of the plane woulde be minished

    採用電力作動器和功率電傳技術作為飛機操縱、環控、液壓、機輪剎車的動力源，減小或取消了集中式的液壓系統，可以使飛機的可靠性和維修性大大提高，重量大大降低。
  15. Based on the flight datum of a300, the mathematical models and the normal control law of uav are built. separating the traditional flight control surfaces into several independent portions, we can reduce the influence of the control surface each and add redundance to the systems at the meanwhile

    採用將傳統操縱面分離成為各自獨立的操縱面的方法，提高了操縱面的綜合作用效果，因而使無人機具有了傳統飛機所沒有的操縱面控制冗餘。
  16. The game is simple to manipulate, above and below key corresponding to the four aircraft lateral movement, the space bar for a shot, based space link can be automatically fire

    游戲的操縱方法很簡單，方向鍵上下左右分別對應飛機的四側移動，空格鍵為發射子彈，按著空格不放可以自動連發。
  17. Abstract : two computational techniques for inverse fight dynamics, namely derivation - iteration and integration - iteration techniques, are investigated. the application of inverse dynamics to determine control power requirements for post - stall maneuvering is researched, and a maneuvering flight trajectory based algorithm is provided, which lays a numerical foundation for simplifying design criteria for post - stall aircraft. with the model of inverse dynamics employed, a flight control mode for the outermost loop of the control system, named maneuver generator, is designed to follow desired complicated maneuvering flight trajectories. an example of rapid heading - reversal maneuver and other numerical simulations show the feasibility of the algorithm and the design idea

    文摘:考察了求解輸入類飛行逆動力學問題的微分-迭代與積分-迭代演算法;探討了利用逆動力學確定過失速機動操縱效能要求問題，這構成了進一步提出過失速機動飛機設計簡化判據的數值基礎;利用逆動力學設計機動發生模塊進行飛控系統的最外環控制，以便跟蹤期望的復雜機動軌跡.飛機最速反向示例及其它數值模擬結果表明設計思想與演算法是可行的
  18. Due to complicated continuous helicopter models and a wide range of constraints, numerical solutions on a mainframe computer have to take a long time. for a given set of initial helicopter states and flight parameters, optimal solutions are fitted by a fourier series. the coefficients of the fourier approximations are then interpolated as functions built by three - layer bp network with inputs of initial flight states and parameters

    最後，由於直升機數學模型的復雜性，這給實時優化計算帶來很大困難，本文研究了地面計算機計算的最優軌跡如何在機載計算機上實時顯示，對飛行員的操縱提供參考，即把不同初始條件得到的最優軌跡曲線進行傅立葉部分級數化，得到傅立葉系數，選取合適初始條件作為變量，對這些最優軌跡曲線進行擬和，建立bp神經網路預測模型。
  19. I watched him manipulating the controls of the aircraft

    我看著他熟練地控制著飛機的操縱儀。
  20. In the airplane, electri - hydro position servo system has principal influence on airplane ' s steering system, while steering system dominates performances of airplane

    飛機的電液位置伺服系統對飛機的操縱系統有著重要的影響，而飛機的操縱系統對整個飛機的性能影響極大。
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