flight control 中文意思是什麼

flight control 解釋
1. （地面對飛機的）飛行指揮，飛行控制。
2. 地面飛行指揮站。

  • 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...
  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. Aerospace ; lock washers for flight control rods

    航空航天.飛行控制桿的鎖緊墊圈
  5. Lqr lqt in design of flight control law

    輸出反饋在飛行控制律設計中的應用研究
  6. Mathematical model of self - repairing flight control

    自修復飛行控制的數學模型
  7. Description of integrated flight control technology

    飛行綜合控制技術淺析
  8. Dissimilar redundant flight control computer system

    非相似余度飛控計算機
  9. Key then used, the flight control around key direction

    然後用上鍵飛翔，左右鍵控制方向。
  10. The next flight control keys around, the space bar shooting

    上下左右鍵控制飛行，空格鍵射擊。
  11. Some flight course switch rules are researched. uav ’ s launch stability and flight course precision are influenced by wind. through the research of flight control, some way are found to lower the wind influence

    研究了風速對無人機的發射穩定性影響，通過風速對無人機導航控制影響的分析，提出了減小側風影響的控制策略，並推出一種計算平均水平風速的方法。
  12. 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。
  13. Matlab / stateflow has a power function of logical management. flight manage system can be edited by stateflow with complex logical management. through the system uav can fly independently or fly by remote control. a power window to display the number and flight course is edited by matlab / gui, through the window flight control parameters and flight state can be adjusted

    利用stateflow強大的邏輯和圖形化編程功能模擬了無人機的飛行管理器，實現了自主飛行和遙控飛行的功能;利用gui用戶圖形界面建立了功能強大的人機界面，對simulink中的模擬數據進行顯示。
  14. 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
  15. 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。
  16. Based on the simulation system software, navigation and guidance real - time digital simulation system are developed to simulate the whole real - time flight control and guidance process

    本文利用vpm平臺，建立運載火箭迭代制導系統的導航和導引模型，形成模塊化的數字模擬系統。
  17. Generation of testing case for model based flight control software of unmanned aerial vehicle

    基於模型的飛行控制軟體測試用例的生成
  18. Development of electromechanical actuation system for flight control is one of the most important technologies in the path to all - electric airplane

    摘要飛行控制中機電作動系統的發展是全電飛機的重要技術之一，而高速大功率密度的無刷直流電動機是其中的關鍵部件。
  19. The final software has four function levels and can run in three different modes : flight control, test end parameters tuning

    最終設計的飛行控制軟體具有4個功能層次，能夠在飛控、測試和調參3種模式下運行。
  20. 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。
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