飛行載具 的英文怎麼說

中文拼音 [fēihángzǎijù]
飛行載具 英文
air
  • 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...
  • 載 : 載Ⅰ名詞（年） year : 一年半載 six to twelve months; six months to a year; 三年五載 three to five ...
  • 飛行 : flight; flying; aviate; voyage; volitate; hop
  • 載具 : rov
  1. Establishing an human spine dynamic model is an significan event to study spine injured biomechanics of pilot " s ejective injury, parachute opening, landing and study the endurance to impact loading on human spine. in this paper, the huston " s method of kane " s equations is developed so that it can be applied to the multibodysystem including translation between the bodyies. the dynamic model of human spine is provided basing on these theories, while the big movement of spine is considered. the deformation of vetebra is far smaller comparing with the intervetebra disc, so the spine is considered into multibodysystem including rigid bodies ( vetebra ) and the flexible bodies ( intervetebra disc ). the computer solution correspond with the results of the large scale human impact test. the rigid coefficient factors and the damping factor of intervetebra joints are obtained

    人體脊柱動力學模型的建立對研究飛行員彈射救生、傘兵跳傘開傘、著陸等脊柱損傷的生物力學以及研究人體脊柱耐受沖擊載荷的極限問題都具有重要意義.首先發展了凱恩方程的休斯頓方法，使其可應用於變形體連接的多體系統，並以此理論為依據建立人體整椎脊柱沖擊動力學模型，此時考慮脊柱的大位移運動，每個椎骨的變形相對椎間盤的變形小得多，把脊柱看成由剛體（椎骨）和變形體（椎間盤）組成的多體系統.並以大型真人坐姿沖擊實驗結果進行了擬合，最後得到腰椎間關節剛度系數因子和阻尼系數因子
  2. Wing - in - surface effect crafts belong to a class of transport vehicles, which make use of the ground effect to fly

    地效飛機是一種主要利用地面效應提供支承力而飛行的運載工具。
  3. Abstract : wing - in - surface effect crafts belong to a class of transport vehicles, which make use of the ground effect to fly

    文摘:地效飛機是一種主要利用地面效應提供支承力而飛行的運載工具。
  4. With the ground effect, they own higher lift / drag ratio than general aircraft, so need less thrust power and have the ability to carry more loads or fly longer

    在地效的作用下，它的升阻比比一般的飛機大，因而飛行時所消耗的推進功率小，具有更大的載重量或航程。
  5. As a two-stage vehicle, the saturn i had full orbital capability for a variety of payloads.

    作為一個兩級飛行器的「土星」具有可將不同有效載荷送入軌道的能力。
  6. The evolution course of chinese solid rocket propulsion technology for space missions since 1950s is presented. the technical features, development process, ground tests and flight records of nine typical solid motors are described. these motors were developed for sounding rockets, upper stages of launch vehicles and orbit transfer systems in application satellites respectively. the evolution of basic technology of chinese solid rocket motors and future developing concept are briefly introduced. the information in the paper are all based on the published literatures

    敘述了20世紀50年代以來中國航天固體火箭推進技術的發展歷程，介紹了9種最具代表性的固體火箭發動機的技術特徵、研製過程、地面試驗和飛行情況，這些發動機分別應用於中國的探空火箭、運載火箭上面級和應用衛星變軌系統.文中還簡要地評述了中國固體推進各單項技術的發展水平
  7. Abstract : the evolution course of chinese solid rocket propulsion technology for space missions since 1950s is presented. the technical features, development process, ground tests and flight records of nine typical solid motors are described. these motors were developed for sounding rockets, upper stages of launch vehicles and orbit transfer systems in application satellites respectively. the evolution of basic technology of chinese solid rocket motors and future developing concept are briefly introduced. the information in the paper are all based on the published literatures

    文摘:敘述了20世紀50年代以來中國航天固體火箭推進技術的發展歷程，介紹了9種最具代表性的固體火箭發動機的技術特徵、研製過程、地面試驗和飛行情況，這些發動機分別應用於中國的探空火箭、運載火箭上面級和應用衛星變軌系統.文中還簡要地評述了中國固體推進各單項技術的發展水平
  8. 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。
  9. Studies on the mechanisms of postflight cardiovascular deconditioning and its countermeasures have important theoretical and practical implications to fully unravel the cardiovascular effects of microgravity and to realize the manned - spaceflight project in the new millennium

    航天飛行后心血管失調發生機理及其對抗措施研究對闡明微重力心血管影響基本規律及實現新世紀載人航天目標具有重要的理論與實際意義。
  10. M95 should not be able to shoot the cockpits of friendly aircraft

    M95將不能穿透友軍飛行載具駕駛艙？
  11. Because of the periodicity of the hub oscillatory load and the nonlinearity of the i / o relationship of the smart rotor, the neural control methods with both off - line and on - line modeling in frequency domain on the smart rotor and their realization procedures are presented

    飛行中直升機的槳轂交變載荷以周期性的為主，而智能旋翼的輸入輸出關系具有非線性特徵。據此，本文提出離線建模的和在線建模的智能旋翼頻域神經控制方法，並給出實現的具體方案細節。
  12. Through this contact, she is sent many codes by which to build a transport to travel to the planet vega

    通過這次的接觸她收到許多密碼，包含了如何製造一具飛行船乘載人到織女星。
  13. While slow flying in the air, hot balloons becomes a focus of observation of people on the ground, actting as remarkable carrier for advertising

    在空中緩緩飛行的熱氣球，是地面上視覺范圍內所有人注目的焦點，因此它成為了最具轟動效應的空中廣告載體。
  14. As far as the system observation for accuracy evaluation of carrier rocket is concerned, there may exist different types of observed data and priors. heterogeneous information means that the different information describing the different characteristics of the same object. since all of the information is relevant to the same object, the fusion is possible. it is a key problem that how to fuse the heterogeneous information to obtain the better evaluation result. therefore, the different heterogeneous information and data is thoroughly studied, moreover, the mathematical description for information fusion of different parameter priors and data is constructed in this paper. based on their relationship between different parameters, indirect prior and observation data is transformed into prior in impact point observation space, which is fused with original prior by weight determined by maximum entropy rule to obtain the mixed posterior distribution. therefore, the test results can be given by combining posterior distribution and impact error observed data. then its application on evaluating guidance systematic error is elaborated as it applies trajectory tracking data, test value of coefficients of guidance instrumentation systematic error, impact point observation data and prior. especially, the advantage of this method lies in its application in case that guidance instrumentation systematic error may not be computed precisely. finally a detailed example on evaluation of carrier rocket is given to verify the theory

    為充分利用運載火箭觀測中的不同觀測空間和過程的信息來進行精度評估，針對該背景建立了異質先驗融合的數學描述.研究了飛行試驗中不同觀測空間和過程的異質先驗信息和數據，基於不同觀測過程的解析關系，將間接過程的先驗和觀測數據算出的后驗分佈轉換成落點觀測空間上的先驗，與原落點的先驗進行了最大熵加權融合，得到混合后驗分佈，從而結合落點觀測數據給出評定結果.在無法解算出精確的制導工具誤差系數的情況下，這種方法充分利用了彈道跟蹤數據、工具誤差系數的地面測試先驗值、落點先驗及落點數據，穩健性更好，準確性更高
  15. Nevertheless, some manned flight mission requires the spacecraft has high pointing and stabilizing precision. so, it needs us to quantitatively analyze the astronautic disturbances, so as to evaluate flight mission and guide or improve spacecraft system design especially the attitude control system design

    有的載人飛行任務需要航天器具有很高的指向精度和穩定度，這就需要對航天員的擾動進行定量分析，以便對飛行任務進行評估並能指導或改進航天器系統設計特別是姿態控制系統的設計。
  16. This space flight allows china to join the space club, and the space industry is much more porfitable than selling plastic toys and shoes in the long term

    這次載人飛行使中國成為世界航天俱樂部中的一員，而從長遠來看，航天工業遠比出口塑料玩具和鞋帽的利潤高得多。
  17. The space station system inosculates the technology of satellite and manned flight vehicle. it can realize manned flight in the low orbit with more reliability, maintainability, expandability and usability

    空間站系統融合了衛星和載人飛船的技術，可以長期在空間低軌道上作載人飛行，而且具有較高的可靠性、維修性、可擴展性和實用價值。
  18. For smaller vehicles with high acceleration the wind may be little concern with structural loads.

    對于具有高加速度的小型飛行器，風與結構載荷的關系可能不大。
  19. The parallel robot has become a hot spot for a long time because of its simple structure, high stiffness, high precision, and low movement inertia. it especially adapted to the task, which required high precision, heavy load and limited space

    並聯機器人具有結構簡單、剛度好、定位精度高、動態響應快等優良特性，特別適用於高精度、大載荷且工作空間較小的場合，在裝配生產線、高精密機床、飛行模擬器、衛星天線換向裝置等等很多方面都有著巨大的應用價值。
  20. Jium - ming lin, tsang chiang, chen - hung lin, and huan - liang tsai, " general optimal control system design by structure uncertainty description and eigenstructure assignment method ", ieee proceedings of the 5th world congress on intelligent control and automation, june 15 - 19, 2004, pp. 396 - 400

    陳震宇、蔡渙良、藍明華， "整合雷達偵?及無人飛行載具海域偵巡之架構研究" ，第一屆管理與決策2005年學術研討會，嘉義南華大學， 2005年5月26 27日。
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