flight dynamics 中文意思是什麼

flight dynamics 解釋
飛行動力學
  • flight : n 1 飛行，飛翔；（鷹對獵物的）追趕。2 （候鳥等的）遷徙；飛行的一群。3 （光陰）飛逝。4 （思想等的...
  • dynamics : n. pl. 1. 〈用作 sing. 〉 力學；動力學。2. 動力，原動力。3. 動態。4. 【音樂】力度強弱法。
  1. The model developed here is suitable for the tilt rotor aircraft during hover, transition and cruise. the longitudinal equations of motion provide a foundation for further investigation on tilt - rotor flight dynamics

    文中所建模型具有較高精度，適合於飛行包線內的所有模式，為傾轉旋翼飛機飛行動力學的進一步研究提供了基礎。
  2. This paper relies on country 863 project " taking off levelly, two stage to orbit and transatmosphere flight vehicle system design ", research towed flight dynamics primarily, development for our country air launch technology of carrier rocket, offering the essential technological reserve

    本論文以國家863項目「水平起飛兩級入軌跨大氣層飛行器總體設計」為依託，對牽引飛行動力學進行初步研究，為我國研究運載火箭空中發射技術提供必要的技術儲備。
  3. 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。
  4. Flight dynamics - concepts, quantities and symbols - part 8 : concepts and quantities used in the study of the dynamic behaviour of the aircraft

    飛行動力學.概念量和符號.第8部分:飛行器動力學特性研究用的概念和量
  5. Flight dynamics - concepts, quantities and symbols - part 7 : flight points and flight envelopes

    飛行動力學.概念量及符號.第7部分:飛行點及飛行包線
  6. Applications to aerospace engineering are discussed, including introductory topics in orbital mechanics, flight dynamics, inertial navigation and attitude dynamics

    亦將討論動力學在航太工程上的應用，包含軌道力學，飛行力學，慣性導航與姿態動力學。
  7. Paremeters and symbols of guidedmissile flight dynamics

    導彈飛行動力學參數符號
  8. Summary about inverse problem of helicopter flight dynamics

    直升機飛行動力學逆問題研究綜述
  9. The exploration of flight dynamics problem on aircraft icing

    飛機結冰引起的飛行動力學問題探討
  10. Flight dynamics - concepts, quantities and symbols - part 6 : aircraft geometry

    飛行動力學.概念量及符號.第6部分:飛機幾何參數
  11. Flight dynamics - concepts, quantities and symbols - part 5 : quantities used in measurements

    飛行動力學.概念量及符號.第5部分:測定使用的量值
  12. Flight dynamics - concepts, quantities and symbols - part 1 : aircraft motion relative to the air

    飛行動力學.概念量及符號.第1部分:飛行器相對于空氣的運動
  13. Flight dynamics - concepts, quantities and symbols - part 3 : derivatives of forces, moments and their coefficients

    飛行動力學.概念量及符號.第3部分:力力矩及其系數的導數
  14. Aerospace ; concepts, quantities and symbols for flight dynamics ; aircraft geometry ; iso 1151 - 6 : 1982 status as of 1984 modified

    航空航天.管.概念.飛行動力學的量值和符號.飛行器的
  15. Investigation of flight dynamics of thrust vectoring aircraft using extended continuation methods

    應用擴展連續演算法研究推力矢量飛機動力學特性
  16. Analysis methods and its development about effect of ice accretion on aircraft flight dynamics characteristics

    結冰對飛機動力學特性影響的分析方法及其進展
  17. Topics extend to analysis of both aircraft flight dynamics and spacecraft attitude dynamics, based upon presented principles and equations of motion

    課題擴展分析了航天器飛行動力學和太空船飛行姿態動力學，這些建立在當前的運動理論和方程式上。
  18. According to flight dynamics, a particle model and an attitude model in launching coordinate system and in quasi missile body coordinate system are established, the influence imposed by constant wind, thrust bias of the motor and connection bias are analyzed

    應用飛行動力學理論，建立了發射坐標系與準彈體系下助推段和分離過程質點運動和姿態動力學模型，分析常風干擾、發動機推力偏差和裝配誤差影響等。
  19. A high fidelity real - time mathematical model of a turboshaft engine was developed and included in the helicopter flight dynamics mathematical model

    建立了高精度、實時渦輪軸發動機數學模型以t700發動機為樣例，引入了一個渦輪軸發動機實時數學模型。
  20. The problem is then fed to a nonlinear programming routine to solve for all parameters. the flight dynamics model with yawing motion of uh - 60a is given, scale factors of state variables and control variables are applied based on the consideration of algorithm convergence. then, the optimization of trajectories is expressed as optimal control problem with a performance index constrained by helicopter performance limits, faa regulation and so on

    首先，建立帶偏航運動的直升機點質量模型，然後對狀態變量和控制變量進行無量綱處理，因為狀態變量和控制變量量值相差較大，這使得優化演算法收斂效果變差，所以需要選擇適當的縮放因子，最後把直升機單臺發動機停車后的飛行軌跡表示成一個最優控制問題，即在考慮直升機性能限制和far規范后，指定一個優化性能指標，選擇合適的路徑約束，然後再解最優控制問題。
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