機動飛行條件 的英文怎麼說

中文拼音 [jīdòngfēihángtiáojiàn]
機動飛行條件 英文
maneuvering flight conditions
  • 機 : machineengine
  • 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...
  • 條 : Ⅰ名詞1 （細長的樹枝） twig 2 （條子） slip; strip 3 （分項目的） item; article 4 （層次; 秩序; 條...
  • 件 : Ⅰ量詞（用於個體事物） piece; article; item Ⅱ名詞1. （指可以一一計算的事物） 2. （文件） letter; correspondence; paper; document
  • 機動 : 1 （利用機器開動的） motor driven; motorized2 （權宜; 靈活） flexible; expedient; mobile; manoeuv...
  • 飛行 : flight; flying; aviate; voyage; volitate; hop
  • 條件 : 1. （客觀的因素） condition; term; factor 2. （提出的要求） requirement; prerequisite; qualification
  1. Based on the frequent occurrence of international aerial crimes, the rampancy and cruelty of criminals and the reality of brutal consequence, the essay analyses the features of the crime of aircraft hijacking, the crime of imperiling international civil aerial security and the crime of obstructing international aerial navigation with the component terms from three important international conventions on punishing aerial crimes in order to help people to appreciate the appearance and the essence of typical international aerial crimes deeply, to regard the motion of the crimes and to overwhelm the offence forcefully. based on the core of the legislative status of international civil aerial security, the jurisdiction of the aerial crimes, one emphasis of the article is to clarify concrete clauses on jurisdiction in the three conventions and analyses the important principle of " aut reddere, aut punire ". based on the problems on the jurisdiction of crimes in international society, it quests the implementation of t he principles of jurisdiction, pleading and extradition in the three conventions deeply

    基於目前國際社會航空犯罪時有發生，犯罪分子猖獗狠毒，危害後果十分殘重的現實，本文從國際社會關于懲治航空犯罪的三個重要國際公約（東京、海牙、蒙特利爾公約）中規定的各種航空犯罪的定義入手，深入展開了對劫持航空器罪、危害航空器飛行安全罪、危害國際民用航空機場安全罪的犯罪特徵及其構成條件的分析，以期幫助人們更深刻認識這些典型的國際航空犯罪的表現及其實質，嚴密注視這些犯罪的動向，對其進行及時有力的打擊；鑒于國際民用航空安全法律地位問題的核心是解決航空犯罪的管轄權問題，本文重點闡釋了三個公約關于管轄的具體規定，並側重分析了「或引渡或起訴」的重要原則；鑒于目前國際社會打擊國際航空犯罪管轄方面存在諸多實際問題，本文對公約規定的管轄、起訴、引渡原則的實現方式作了深入探討；鑒于各國在國內立法上對于空中犯罪的懲治、對違約國的制裁、對這類犯罪的預防措施等方面存在一些漏洞，本文根據目前掌握的一些資料，在獨立思考的基礎上，提出了一些不成熟的看法及建議，以期對國際社會懲治航空犯罪貢獻自己微薄之力。
  2. On the basis of introducing the principle of the tf / ar radar, this paper analyzes the conditions of effectively jamming the tf / ar radar in typical tactical act of hedgehopping, which include the disposition and quantity of electron reconnaissance / jammer, calculates the capability request of equipments in the method of sensor / hand - emplaced jammer, and concludes that it is difficult to jam tf / ar radar at the present time

    摘要在介紹地形跟隨迴避雷達工作原理的基礎上，通過設定典型超低空突防飛機的戰術行動，分析了對雷達實施有效干擾所必須具備的條件，包括偵察干擾機的部署、數量要求等；並計算了在傳感器擺放（投擲）式干擾機模式下對裝備的性能要求，得出了在目前技術條件下，對地形跟隨迴避雷達實施干擾在技術和戰術上都是困難的。
  3. In chapter 5, the uh - 1 model rotor, the model rotor measured in the present work and the helicopter z - 8 rotor are taken as numerical examples, the calculations on rotor noise under different flight conditions are carried out for validation purposes

    應用該模型，分別以uh - 1模型旋翼、本文試驗的模型旋翼以及z - 8直升機旋翼為算例，對不同飛行條件下的旋翼氣動噪聲進行了計算，驗證了本文的計算方法。
  4. A integrated flight / propulsion control ( ifpc ) theoretical schema was designed based on this concept and a engineering schema was developed after take consideration of currently engineering condition and the requirements of in - service aircraft upgrade. a auto - flight system was designed which can achieve accurate flight movement control and increase performance of flight task such as ascend, cruise, te

    基於該概念設計了飛推綜合原理方案，並在考慮工程實現條件及現役飛機改進、改型要求后建立了工程實現方案，設計了軌跡跟蹤方式的自動飛行系統，解決了軌跡生成、表示、管理、跟蹤等問題，能夠實現運動狀態的精確控制，提高爬升、巡航等任務的性能。
  5. Virtual instruments technology was applied to build the measurement and control system and develop the software for the experiment, which improve the efficiency of the study. finally the velocity control experiment of sapc at several flight states was accomplished which has a good effect. the study has certain significances on developing electronic - electric cpcs

    構建基於虛擬儀器技術的測控平臺，採用labview軟體開發測控軟體，利用實驗室的現有條件，結合某型電子/氣動式壓調器的實驗，完成了飛機在各種飛行狀態下所需的大氣壓力模擬艙內的壓力控制，取得了較好的效果。
  6. Firstly, the study about flight icing is reviewed at the beginning. the condition of icing accretion, the style of icing accretion, the parameters of icing accretion in flight, and the influence of icing accretion on the aerodynamic characteristics of an airplane are analyzed

    首先，回顧了國內外在飛機結冰方面的研究情況，對飛機在飛行中的結冰條件、結冰類型、結冰參數以及結冰對氣動特性的影響進行了分析討論。
  7. Compared with a delta wing aircraft, the double - delta wing configuration has better aerodynamic performance at high angles of attack. an operational analysis was introduced as a method for evaluating training effectiveness of trainer aircraft. approaches to the engineering estimation of aerodynamic characteristics for aircraft with a double - delta wing configuration were studied, and the procedures for determining aircraft performance indices formulated. taking training effectiveness as the objective function and geometric parameters of the wing platform as design variables, through a numerical multivariate optimization arithmetic, the conceptual design optimization for a certain fighter trainer aircraft with double - delta wing configuration was carried out under the constraints of tactical and technical requirements and interrelated geometry. agreement of a calculation example with engineering practice indicates that the optimal design has higher training effectiveness than the baseline design, and in addition, improves the structural force - bearing conditions

    雙三角翼氣動布局比三角翼飛機具有更好的大攻角空氣動力特性.引入了評估教練機訓練效能的作戰分析法，研究了雙三角機翼布局飛機空氣動力特性的工程計算途徑以及飛機性能指標的確定方法.以訓練效能作為目標函數並選取機翼平面形狀的幾何參數為設計變量，採用多變量數值尋優方法，在戰術技術指標及相關幾何約束條件下，對某高級教練機的雙三角機翼氣動布局方案進行了優化選擇.算例表明最優方案不僅比原準方案具有更高的訓練效能，還改善了結構的受力情況，與工程實踐吻合
  8. 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。
  9. The result control system is demonstrated using post - stall maneuver simulation, the results show that this control law achieves a high level performance in post - stall maneuver conditions even if the aircraft model has large uncertain items

    結果表明，在存在較大模型誤差的情況下，所設計的飛控規律完全能在過失速機動條件下控制飛機跟蹤指令飛行。
  10. The automatic control system, as a critical technology, has an irreplaceable effect in keeping flight security and promoting attack efficiency. so high - qualified flight control system is necessary for completing the complex flight missions

    飛行自動控制系統作為現代飛機的一項關鍵技術，在保持飛機飛行安全和提高攻擊效率方面起著不可替代的作用，所以高性能的武裝直升機的飛行控制系統的設計和使用是保證其完成復雜飛行任務的必要條件。
  11. Standard test method for measurement of thermal stability of aviation turbine fuels under turbulent flow conditions hirets method 1, 2

    在快速流動條件下測定飛行器渦輪機燃料的熱穩定性的標準試驗方法
  12. Through it the author made a deep study of the satellite attitude control subsystem, verified several sorts of disturbance torques and realized satellite three - axis attitude stabilization control and attitude maneuver under different conditions

    本文在simulink下對衛星姿控系統作了比較深入的研究，對各種干擾力矩進行了驗證，同時在不同的模擬條件下實現了衛星三軸穩定控制、姿態機動和飛輪的磁卸載。
  13. In addition, the services are adopting new preservation strategies to keep their aircraft flying in the middle east, where harsh environmental conditions and sand have wreaked havoc on helicopter rotor blades and aircraft engines, avionics and wiring

    除此之外，軍方正在採用新的維護計劃以保證有足夠的飛機在中東飛行，那裡惡劣的環境條件和沙塵將嚴重破壞直升機的旋漿、飛機的發動機以及航空電子設備。
  14. Besides, the design of vane is the major project of the uav research, because the vane is the most important part in power transformation of the uav, the quality of this part will directly affect the capacity of the uav. we should manage to enhance the lift resistance ratio in the same situation

    此外，本課題著重對無人機的葉片部分進行設計，因為葉片是無人機的動力轉化部分，它的好壞直接影響著飛行器的飛行性能，在相同外部條件下，盡可能使其產生比較大的升阻比。
  15. There are great differences between ground test of a flight vehicle ' s aerodynamics and that of a dual - mode scramjet when ground test facilities are used to do experiments on a dual - mode scramjet engine, the components of incoming flow and its parameters, including total pressure, total temperature ( or total enthalpy ) and velocity must be simulated. at the same time, since the fuel ' s resident time within a combustor is very short, on the order of one millisecond, it is difficult to measure the flow - fields

    進行雙模態沖壓發動機地面試驗研究時，必須要求試驗設備能模擬實際飛行條件下來流氣體的組分、總壓、總溫（或總焓）以及來流氣體的流動速度；同時由於燃料在燃燒室內駐留的時間很短，一般為毫秒量級，從而使流場物理量的測定顯得非常困難。
  16. Three axis optical tracking test table is a kind of powerful instrument used to reproduce the flying posture of flying weapons in laboratory. the test table, together with equipment producing target, simulates the attacked target and flying missile, which can really simulate the various flying postures in space and dynamic characteristics. thus, the performance of sensors, control system and actuator and so on can be tested and evaluated, which provides various reference bases for developing, improving and redesigning flying weapons

    三軸光學跟蹤試驗轉臺是一種在實驗室條件下復現飛行器或導彈在空中飛行姿態半實物模擬的有力工具，它和目標發生裝置組合在一起模擬導彈跟蹤目標的過程，可以真實地模擬出導彈等飛行器在空間的各種姿態和動力學特性，從而對其傳感器件、控制系統和執行機構等硬體設備的性能加以測試和評價，為飛行器的研製、改進和再設計提供各種參考依據。
  17. 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。
  18. With the help of adams and simulink ’ s union simulation technology, docking dynamics simulation in the initial conditions ( pose and velocity ) is given. by compare them with the result of the spatial two aerocraft ’ s docking model, principle of loop control system based on dynamics is proofed correct. by compare them with the experiment ’ s result, the virtual prototype model is certified correct

    藉助adams與simulink的聯合模擬技術，在給定對接初始條件（位姿和速度）下，進行了對接動力學模擬，並與空間兩飛行器對接的模擬結果進行了比較，驗證了大迴路控制系統動力學控制原理的正確性;與試驗結果進行了比較，驗證了樣機模型的正確性。
  19. In order to ensure the stable work of fighter planes while increasing their maneuverability, it is necessary to investigate the vibration performance of aero - engine in maneuver flight

    為了確保飛機在提高其機動性能的同時還能穩定工作，不發生故障，有必要對機動飛行條件下的發動機轉子系統的振動特性進行研究。
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