空氣動力飛行器 的英文怎麼說

中文拼音 [kōngqìdònglìfēihángqì]
空氣動力飛行器 英文
aerodynamic vehicle
  • 空 : 空Ⅰ形容詞（不包含什麼; 裏面沒有東西或沒有內容; 不切實際的） empty; hollow; void Ⅱ名詞1 （天空） s...
  • 氣 : Ⅰ名詞1 （氣體） gas 2 （空氣） air 3 （氣息） breath 4 （自然界冷熱陰晴等現象） weather 5 （氣味...
  • 力 : Ⅰ名1 （力量; 能力） power; strength; ability; capacity 2 [物理學] （改變物體運動狀態的作用） forc...
  • 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...
  • 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...
  • 器 : 名詞1. （器具） implement; utensil; ware 2. （器官） organ 3. （度量; 才能） capacity; talent 4. （姓氏） a surname
  • 空氣 : 1 （大氣） air; atmosphere 2 （氣氛） atmosphere 3 （氣閘） air brake4 pneum ; pneumo ; pneumat ;...
  • 飛行器 : aerobat; air vehicle; beast; bird; flight vehicle
  • 飛行 : flight; flying; aviate; voyage; volitate; hop
  1. It is an important half hardware - in - loop simulation equipment, which is often used to simulate the aerodynamic torque load on the missile rudder or elevon actuators in the flight

    它是地面半實物模擬系統中的一種重要專用設備，用來模擬飛行器舵機在飛行過程中所承受空氣動力力矩載荷。
  2. "aerodynamics" defines the pressure fields and loads that exist on a launch vehicle due to the reaction of ambient flow.

    「空氣動力學」規定了由於繞流反作用在發射飛行器上存在的壓力場和載荷。
  3. The first successful sustained powered flights in a heavier - than - air machine were made here by wilbur and orville wright on december 17, 1903

    1903年12月17日，萊特兄弟第一次用比空氣重的飛行器進行了有動力的持續飛行。
  4. The first succes * * * ul sustained powered flights in a he * * * ier - than - air machine were made here by wilbur and orville wright on december 17, 1903

    1903年12月17日，萊特兄弟第一次用比空氣重的飛行器進行了有動力的持續飛行。
  5. Research on the aerodynamic interaction between the rotors and components of rotorcraft have been a very important aspect and a very challenging subject in rotorcraft aerodynamics

    旋翼干擾空氣動力學問題一直是旋翼飛行器空氣動力學的研究熱點和難點之一。
  6. The conformal array is usually allocated on an aircraft, missile, or some other mobile platform conforming the shaped surface. its major advantage is the aerodynamic of aircraft is almost not changed

    共形陣列常安裝在飛行器或其他移動平臺載體表面，具有不改變飛行器表面空氣動力學性能，簡化天線安裝等優點。
  7. Load simulator was an important simulation system in hardware - in - loop flight simulation laboratory, which could simulate aerodynamic loads acting on flight vehicle, such as unmanned aerial vehicle, planes

    負載模擬器是半實物模擬實驗室中模擬無人機等飛行器在飛行中舵面所受空氣動力載荷的重要設備。
  8. Electro - hydraulic servo loading system ( ehsls ) is an important simulation system in hard ware - in - loop flight simulation laboratory, which can simulate aerodynamic loads acting on flight vehicle, such as missiles, planes. its performance of test is important on the design of flight vehicle

    電液伺服負載模擬器是半實物模擬試驗室中模擬飛行器在飛行中舵面所受空氣動力載荷的重要設備，它的試驗能力高低對飛行器設計起著重要作用。
  9. Electro - hydraulic servo loading system ( ehsls ) is an important simulation system in hardware - in - loop flight simulation laboratory, which can simulate aerodynamic loads acting on flight vehicle, such as missiles, planes. it is one of most important devices in the whole flight vehicle simulation system

    電液伺服加載系統是半實物模擬實驗室中模擬導彈等飛行器在飛行中舵面所受空氣動力載荷的重要設備，它是飛行器大迴路半實物模擬系統的重要組成部分。
  10. It is essential therefore to explore the aerodynamic aspect of the subject in some depth before proceeding to particular studies of vehicle dynamics.

    因此，在進行飛行器動力學的專門研究之前，有必要對該問題的空氣動力學方面作一定深度的探討。
  11. Aerodynamics - concepts, quantities and symbols. part 2 axis systems and aircraft motion state quantities

    空氣動力學概念量和符號第2部分坐標軸系和飛行器運動狀態量
  12. Electro - hydraulic servo loading system ( ehsls ) simulates the aerodynamic torque acting on the rudders while flying. ehsls can be used to create various types of loading on the rudders in the lab condition to analyze its performance

    電液伺服加載系統是模擬飛行器在飛行過程中舵面所受空氣動力矩的加載裝置，其功能是在實驗室條件下復現飛行器舵面所承受的各種氣動載荷。
  13. Aerodynamics - concepts, quantities and symbols. part 3 aircraft geometry

    空氣動力學概念量和符號第3部分飛行器幾何特性
  14. This article introduces the design and implement of flight simulator based on dsp which contains five parts. the first part establishs the math model of flight simulator which contains the model of aerodynamics and flight mechanics, the model of standard atmosphere and wind model ; the second part introdces primarily the arithmetic of numeric integral which is very important to dyanmic system simulant. the third part introduces the design of hard interface circuit and program. the fourth part introduces the data flow graph of the flight simulator software and gunge - kutta integral arithmetic. the finall part introduces the design of serial port communication software, it contains communication protocol, the process of upper machine and lower machine communication and the programing of serial port communication by vc + +

    本文介紹了基於dsp的飛行器模擬器設計與實現，主要分為五個部分，第一部分建立了飛行模擬的數學模型，包括飛行器空氣動力學和飛行力學的數學模型、標準大氣模型和風模型；第二部分主要介紹了數值積分演算法，它在動態系統模擬中是很重要的；第三部分為硬體介面設計與編程；第四部分介紹了氣動模擬軟體的數據處理流程和runge - kutta積分演算法；最後一部分為串口通信軟體設計，介紹了通信協議、上下位機處理流程和vc + +串口通信編程。
  15. This group focus on the research of missile and launch vehicle, which contain the guidance law and the controller design. there are two researchers in this group now, including one m. d

    本研究群的宗旨乃進行攔截飛彈及運載火箭之研究，主要包含導引法則及自動駕駛儀控制器設計等項目，並利用各式各樣的模擬（其中也包含空氣動力學模型） ，驗證其系統可行性。
  16. In the modeling of dynamics of the vehicle, the forces and moments arise from both aerodynamic and propulsive sources, which are for these configurations hard to separate

    模型建立中，由於由推進系統以及空氣動力產生的力與力矩很難分離，因此本文只是提出一個設計初級階段考慮飛行器特性的解析表達式。
  17. Control system design for hypersonic vehicles will be complicated by coupling effects between aerodynamics, propulsion, and structure

    高超聲速飛行器的飛行控制系統由於空氣動力學、推進系統以及結構之間的相互耦合影響而變得非常的復雜。
  18. The pressure model of flush airdata sensing system is nonlinear equations of the angle of attack, angle of sideslip, dynamic pressure and static pressure of the free stream

    飛行器表面的壓力分佈是大氣數據（迎角、側滑角、動壓、靜壓）的非線性函數，這個函數主要可以從空氣動力學模型得到。
  19. In this paper, dynamic inversion control law is designed to eliminate its global non - linearization and unstable aerodynamic force etc. and based on the time - scale separation principle, the control system can be divided into fast loop and slow loop. but there are still lots of unknown disturbances that may cause great damages to stability when flying

    由於在飛行過程中大范圍非線性、具有非定常氣動力等特性，本文採用了非線性動態逆控制律來構成全局線性化的性質，根據時標分離的原則，設計了空天無人飛行器的快迴路和慢迴路控制器。
  20. Load - simulator is a device developed to test the performance of rudder control system in the lab by simulating and applying air moment the rudder suffering. high performance load - simulator is in urgent need for the examination of newly developed aircrafts and control techniques

    負載模擬器是模擬飛行器等在飛行過程中舵面所受空氣動力矩的加載裝置，其功能是在實驗室條件下復現飛行器的舵面在空中所受的各種載荷，從而檢測其舵機驅動系統的技術性能指標。
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