flight control system 中文意思是什麼

flight control system 解釋
飛機操縱系統
  • 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...
  • control : n 1 支配,管理,管制,統制,控制;監督。2 抑制(力);壓制,節制,拘束;【農業】防治。3 檢查;核...
  • system : n 1 體系,系統;分類法;組織;設備,裝置。2 方式;方法;作業方法。3 制度;主義。4 次序,規律。5 ...
  1. Flight control system ( fcs ) sensor is used for measuring various kinds of mobile parameters of aerocraft, describing its mobile state and spacial position. it is the principal subunit in the fcs

    飛控系統傳感器用於測量飛行器的各種運動參數,描述飛行器的運動狀態及其在空間的位置,是飛行控制系統的首要環節。
  2. 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。
  3. Because these wind loads are a major structural consideration, they greatly influence the design of the flight control system.

    因為這些風載荷是結構上主要的考慮因素,它們很大地影響著飛行控制系統的設計。
  4. When testing begins, the computer of the tested uav flight control system will be connected into the network as a slave. the master of the system will diagnose faults should there be any ; otherwise it will set flight parameters and load flight course data for the slave

    檢測時,無人機的飛控系統計算機作為從機連入網路,如果從機的飛控系統沒有故障,主機將為從機設置飛行參數和裝定航線數據;如果有故障,則主機為從機飛控系統診斷故障。
  5. Helicopter is hard to hover precisely for its bad stability. ordinarily, it is improved by flight control system, such like rotorcraft unmanned aerial vehicles which use bell bar or bell - hiller stabilizer bar. bell stabilizer bar, fixed across with teetering main rotor, consists of a bar and masses at two ends

    貝爾穩定桿由一桿與兩質量塊組成,它與貝爾直升機的蹺蹺板旋翼垂直交叉放置,這種旋翼裝置有助於加大角速度阻尼,改善貝爾直升機的穩定性,但同時也降低了操作性。
  6. 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。
  7. 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。
  8. Fly - by - wire flight control system

    電傳飛控系統
  9. 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。
  10. Study on intelligent flight control system based on genetic algorithm and fuzzy logic control

    基於遺傳演算法和模糊邏輯的智能飛控技術研究
  11. 3 ) definition of input designer concept for flight control system ( fcs ). a input designer was successfully constructed which can provide a effect almost the same as directly control over aerodynamic control surface through the careful design of inputs of fcs. this input design concept is very important for in - service aircraft upgrade where change of the original pcs is not allowed

    3 )提出了飛控系統輸入設計概念,並成功地構建了飛控輸入設計器,能夠在不改變原飛控系統條件下有效地提高舵面控制能力,獲得接近直接舵面操縱的性能,對于現役飛機改進、改型中飛機運動自動控制系統的設計具有非常重要的意義。
  12. 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
  13. For example, finger - on - glass controls replace cockpit switches for selecting such functions as air refueling mode and flight control system tests

    舉個例子,指觸屏幕控制技術取代了選擇諸如空中加油模式和飛行控制系統檢測等相應功能的座艙開關。
  14. 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。
  15. Then above the typical terrain and under the disturbance the terrain following system is simulated. the result shows the flight control system can withstand the disturbance and track the optimal trajectory

    在典型地形情況下進行地形跟隨模擬,並且為了真實模擬地形跟隨,在控制通道加入風擾動,結果表明該飛控系統能夠很好的抵抗風擾動,緊緊跟隨最優軌跡飛行。
  16. 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。
  17. 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。
  18. 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。
  19. Then according to system simulation technology, the overall air - to - ground attack simulation plan is made with the thought of models and layers. after that, the mathematical models of main parts in the simulation are made such as aircraft body, propulsive system, flight control system, fire control system, bomb and air - to - ground missile. on the basis of these mathematical models, using the object - oriented design methodology, a set of air - to - ground attack real - time visual simulation software is developed. this software can be used to aid aircraft design, research of air - to - ground attack tactics and flight training

    本文首先介紹了現代戰爭中空對地攻擊的技術裝備及其特點,計算機模擬技術的發展以及面向對象的軟體設計思想;而後使用系統模擬技術,依據分層、模塊化設計思想,制定了空對地攻擊模擬系統總體設計方案;之後根據目前技術狀況,建立了戰斗機機體、推進系統、飛控系統、火控系統、航空炸彈、空地導彈等子系統數學模型;在此基礎上,利用面向對象的軟體設計思想,在基於pc的平臺上開發了一套對地攻擊視景模擬軟體,實現了戰斗機對地攻擊實時視景模擬。
  20. Introduction to flight control system of small unmanned helicopter

    小型無人直升機自主控制系統介紹
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