飛機控制系統 的英文怎麼說

中文拼音 [fēijīkòngzhìxìtǒng]
飛機控制系統 英文
acs aircraft control system
  • 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
  • 控 : 動詞1 （告發;控告） accuse; charge 2 （控制） control; dominate 3 （使容器口兒朝下 讓裏面的液體慢...
  • 制 : Ⅰ動詞1 （製造） make; manufacture 2 （擬訂; 規定） draw up; establish 3 （用強力約束; 限定; 管束...
  • 系 : 系動詞（打結; 扣） tie; fasten; do up; button up
  • 統 : Ⅰ名詞1 （事物間連續的關系） interconnected system 2 （衣服等的筒狀部分） any tube shaped part of ...
  • 飛機 : airplane; plane; aeroplane; kite; bird; aircraft
  • 控制 : control; dominate; regulate; govern; manage; check; cybernate; manipulate; encraty; rule; rein; c...
  • 系統 : 1. （按一定關系組成的同類事物） system 2. （有條理的;有系統的） systematic
  1. The research and development of flight control system is not dissociable with simulation technology. simulation has become an important tool for successful development of flight control system of unmanned helicopter

    無人直升機飛行控制系統的研製已和模擬技術密不可分，模擬已成為無人直升機飛行控制系統研製成功的必要手段。
  2. Design of flight control appliance used in minitype pilotless aircraft

    小型無人飛機控制系統的飛行控制器設計
  3. The modern unmanned helicopter flight control system is generally composed of the flight control computer, the servo driving mechanism, the sensor, and the ground monitor control system etc. in this thesis the research to the helicopter flight characteristics was conducted at first, and its flight dynamic model was preliminary discussed, especially the mathematic model under hung - stop condition was formulated and the algorithm of the controller was designed in detail

    現代無人直升機飛行控制系統一般由飛行控制計算機、伺服驅動機構、傳感器、地面監測控制等分系統組成。本文首先對直升機的飛行特性進行了研究，並且對飛行動力數學模型做了初步探討，尤其對在懸停狀態下的數學模型做了較為詳盡的公式推導和控制器的演算法設計。
  4. This paper focuses on the flight simulation research of flight control system of unmanned helicopter

    本文就是針對無人機飛行控制系統中飛行模擬這一環節進行研究的。
  5. Self - repairing flight control system ( srfcs ) is a kind of active - and passive failure tolerant control based on the fly - by - wire flight control system, and it is also an important tendency of the future flight control system

    自修復飛行控制系統（ srfcs ： self - repairingflightcontrolsystem ）是在電傳飛控系統基礎上發展起來的一種與主動容錯技術結合的先進飛控系統，也是未來戰斗機飛控系統的重要發展方向。
  6. The application of parameter space method in design of flight control system for tiltrotor aircraft

    參數空間法在傾轉旋翼機飛行控制系統設計中的應用
  7. But fcs and " fly / fire " coupler is the key technique of iffc 。 in this paper, a fire control system of armed helicopters for ground attack is proposed based on the attack system of fix - wing. we stress on our research of fcs, iffc and " fly / fire " coupler for armed helicopters

    本文在參考固定翼飛機攻擊系統的基礎上，建立武裝直升機對地攻擊的火控系統，重點對直升機飛行控制系統、綜合飛行/火力控制系統、以及飛行/火力耦合器等進行了研究。
  8. Flight control system and propulsion control system are two of important control systems on an aircraft

    飛行控制系統和推進控制系統是飛機上兩個重要的控制系統。
  9. On the basis of designing robust flight control system of the new generation fighter, this dissertation is devoted to the design of the integrated fire / flight control system and the integrated flight / propulsion control system and the integrated fire / flight / propulsion control system

    以研究新一代殲擊機的魯棒飛行控制系統為前提，進一步研究其綜合火力飛行控制系統、綜合飛行推進控制系統以及綜合火力飛行推進控制系統的魯棒控制問題。
  10. The flight control system of attack helicopter and the influence of disturbance during noe flight are studied in this dissertation. and the use of h robust control and dynamic inversion schemes in flight control system are discussed

    本文主要對貼地飛行時武裝直升機的飛行控制系統進行深入的研究和探索，討論了貼地飛行時氣流擾動對直升機系統的影響，研究了h _魯棒控制和動態逆控制在直升機飛控系統中的應用。
  11. Self - repairing flight control system ( srfcs ) is a kind of active and passive failure tolerant control based on the fly - by - ewire flight control system, and it is also an important tendency of the future flight control system

    自修復飛行控制系統（ srfcs ： self - repairingflightcontrolsystem ）是在電傳飛控系統基礎上發展起來的一種與主動容錯技術結合的先進飛控系統，也是未來戰斗機飛控系統的重要發展方向。
  12. This dissertation investigates design of reconfigurable flight control systems of a certain model hale uav which is supported by initiative research project fund of china during the 10th 5 year plan

    本文以我國某型高空長航時無人機預研項目為背景，設計具有高生存力的可重構飛行控制系統，實現單一故障條件下飛機的可靠正常飛行。
  13. Missile rudders are executive bodies of missile flight control system, all kinds of attitude motion of missile are depended on the actuator driver fins of rudders

    導彈舵機是導彈飛行控制系統的執行機構，導彈的各種姿態運動都是靠舵機帶動舵面偏轉來實現的。
  14. Flight control system development for the xv - 15 tiltrotor aircraft

    15傾轉旋翼飛機飛行控制系統概述
  15. Using this method, the flight control law which suits to the vectored aircraft flight in post - stall domain is designed in this paper

    運用這種方法對推力矢量飛機進行了適用於過失速機動的非線性飛行控制系統設計。
  16. In this dissertation the control loop of attitude angle and collective piston loop are separately. the controller is designed at two scales. and the simulation shows the uncoupling of three attitudes angle loop is achieved with dynamic inversion scheme

    在姿態角通道的設計中，採用了動態逆思想，按照時標分離的原則將直升機飛控系統劃分為快慢迴路，並採用動態逆方法對飛行控制系統進行設計和模擬，模擬結果表明動態逆在通道解耦方面非常有效。
  17. In flight test, using the method of system identification, the model of the dropped order is taken, then the performance of control syetem of the drone is evaluated. in order to analysize the precision guidance of the flight test, two method is usedizero time sample test and small sample test

    在飛行試驗中，要對無人機的飛行控制系統的性能進行評估，運用系統辨識的方法，對試驗數據進行辨識，獲得其降階模型，從而對其性能進行評估。
  18. 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。
  19. First, to research the reconfigurable flight control system, a flight simulation system of normal aircraft with normal flight control law is established

    首先，為了自修復飛行控制系統研究，建立了具有正常飛行控制律的正常飛機飛行模擬系統。
  20. The thesis describes the conception of the object - oriented modeling and integrated simulaton enviroment, and discusses the below topics : ( 1 ) describe the reasonable structure of the modern fighter simulation system, and design the data transfer interface. ( 2 ) discuss the modeling method of the key subsystem of future fighter system especially the aerodynamics and the control system in detail. ( 3 ) construct the 3d model of the aircraft and scene, and verify the graphic simulation technique based on pc

    本文詳細討論了面向對象建模方法以及一體化模擬環境的基本概念框架及基本結構並在此基礎上提出了合理的現代戰斗機模擬系統結構，設計了模擬系統的數據傳遞介面；詳細討論了現代戰斗機模擬系統關鍵子系統? ?飛機本體、飛行控制系統建模方法；建立了用於研究的飛機以及視景的三維顯示平臺；並在此基礎上實現了實驗性的基於pc的現代戰斗機圖形模擬平臺，對模擬模型有效性確認和驗證工作做了初步的探討，研究比較了傳統飛行動力學和運動學方程和四元數法在飛行模擬中的效果。
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