飛機操縱面 的英文怎麼說

中文拼音 [fēijīcāozōngmiàn]
飛機操縱面 英文
flight control surface
  • 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
  • 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...
  • 面 : Ⅰ名詞1 （頭的前部; 臉） face 2 （物體的表面） surface; top 3 （外露的一層或正面） outside; the ri...
  • 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. Design of innovative control surfaces of flying wing aircrafts with large ratio aspect

    大展弦比飛翼布局飛機新型操縱面設計
  2. 3 ) definition of input designer concept for flight control system ( fcs ). a input designer was successfully constructed which can provide a effect almost the same as directly control over aerodynamic control surface through the careful design of inputs of fcs. this input design concept is very important for in - service aircraft upgrade where change of the original pcs is not allowed

    3 ）提出了飛控系統輸入設計概念，並成功地構建了飛控輸入設計器，能夠在不改變原飛控系統條件下有效地提高舵面控制能力，獲得接近直接舵面操縱的性能，對于現役飛機改進、改型中飛機運動自動控制系統的設計具有非常重要的意義。
  3. On semi - active aircraft flutter control by er fluid damping pivot

    電流變液在飛機操縱面顫振半主動控制中的應用研究
  4. According to the fault type of the flight control surfaces, they are classified and modeled

    文中對飛機操縱面可能出現的故障進行分類，建立數學模型。
  5. 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。
  6. This paper presents a simulation test control system of an airplane engine operating system, which control motor to simulate the force and velocity of throttle lever and the torque on axis

    本文闡述了某型飛機發動機操縱系統地面模擬試驗控制系統，它主要控制力矩電機去模擬油門桿上的速度和力以及模擬發動機輸入軸的力矩。
  7. Direct side force control ( dsfc ) comes into being with the appearance of act ( active control technology ). through maneuvering the vertical canard to produce side force, people can control a aircraft easily. so the trajectory of a vehicle can be controlled precisely, and it ' s maneuverability is greatly improved

    直接側力控制是隨著主動控制的提出而出現的，採用直接側力控制，可在不改變飛機姿態的條件下，直接通過控制面造成側力來操縱飛機機動，從而達到精確控制飛行軌跡和增強機動能力的目的。
  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. And flight - simulator fans can simulate the view from an aircraft ' s cockpit windows

    同樣飛行模擬的愛好者也可以用其來模擬飛機操縱艙中不同方向上的幾面窗戶。
  10. For the past decades, many efforts have been made to learn the behaviors of landing gear during touchdown. with these known behaviors of landing gear, a number of methods have been developed to attenuate the landing impact loads

    作者實現了某型運輸機起落架和全機得數字化虛擬樣機，不但能夠真實模擬飛機著陸性能，而且從系統的高度為靜平衡、滑跑和地面操縱等性能模擬提供了良好的平臺。
  11. 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。
  12. The subsystem is integrated in the cad system of catia, and applies kinematics 3d - manikin and mechanics 3d - manikin in different phase of aircraft cockpit design, and acquires perfect kinematics and mechanics results of pilot. the subsystem whose interface is friendly and utilization is directly, enriches the methods by which the designer estimates an aircraft cockpit design, and enhances the design efficiency and precision

    該子系統集成在catia系統中，在飛機座艙設計的各個階段分別引入了飛行員三維人體幾何模型和運動學模型，通過模擬飛行員的操作動作與計算視角、可達性、操縱力等參數，較好的反映了飛行員的運動學和動力學特徵；界面友好，操作直觀、簡便；豐富了設計人員對飛機座艙設計評估手段，保證了設計效率和精度；有利於飛機座艙設計水平的提高。
  13. In a book written by an electronics expert who once participated in the us star wars program, the author discussed his findings in his studies on several fallen ufos unidentified flying object. according to him, ufos do not look very big from the outside, but after entering them, one might spend twenty minutes walking without reaching the opposite end due to a conversion of time and space. unlike an aircraft cockpit with dashboards and maneuvering devices, the ufos have only a few seats, surrounded by walls which themselves serve as jumbo tv monitors

    他在對多種墜落的幽浮外星人飛行器考察研究時發現，從外面看幽浮並不很大，但進去后卻走二十多分鐘走不到頭時空轉換，而且裏面沒有像飛機駕駛艙內那樣眾多的儀表及操縱裝置，只有幾個坐椅，四周的墻壁就是大屏幕觀測電視，內部也沒有復雜的集成電路，只有大的晶體塊，整個飛行器完全是在外星人頭腦發出的電磁波控制下運行。
  14. Moreover, aircraft actually generate several vortices ? off the tail flaps, control surfaces and other areas of air - pressure discontinuity, states alan j

    此外，連續體動力學公司的總裁畢拉寧說，飛機其實會產生好幾個渦流- -尾襟翼、操縱面與其他產生氣壓不連續的區域。
  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. 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。
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