transition flight 中文意思是什麼

transition flight 解釋
改裝飛行
  • transition : n 轉變，演變，變遷，變化；飛越；過渡期；【音樂】變調，轉調；【修辭學】語次轉變；【語法】轉換；【...
  • 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...
  1. The model developed here is suitable for the tilt rotor aircraft during hover, transition and cruise. the longitudinal equations of motion provide a foundation for further investigation on tilt - rotor flight dynamics

    文中所建模型具有較高精度，適合於飛行包線內的所有模式，為傾轉旋翼飛機飛行動力學的進一步研究提供了基礎。
  2. Scramjet combustor may realize the subsonic - combustion mode and supersonic - combustion mode respectively based on the control of fuel in variable flight conditions. isolator has great effect on mode transition and preventing unstart of inlet. inlet can be unstarted by raising the back pressure result from chemical energy release in the combustor

    計算研究表明，在相同的來流條件下，供油規律對燃燒室的工作模態有著重大的影響；在不同的來流條件下，可以通過調節供油規律使燃燒室分別實現亞燃模態和超燃模態；隔離段對防止燃燒引起的壓力升高對進氣道的干擾和燃燒室的模態轉換具有重要的作用。
  3. Design of automatic transition and hovering flight control system for helicopter

    直升機自動過渡懸停飛行控制系統設計
  4. The application of control law developed above to the problem of reconflgurable flight control is described. based on the simulation results, the effects of learning rate ( or adaptation gain ) and slide model terms on the control system are discussed. comparing with adaptive control, the control law is helpful to improve system ' s transition response and reduce undesirable oscillations, provides nearly perfect tracking in the case of undetected failure

    4 、探討了所設計的控制律在重構飛行控制中的應用，討論了自適應調整率對自適應控制性能的影響、滑模魯棒控制補償項對控制性能的影響；對幾種舵面損傷的模擬結果表明，本文的控制律較自適應控制具有響應改善速度快、響應振蕩小的優點，具有較好的重構功能。
  5. It has conducted an analysis of the virtual aircraft instrument system, finds out the characteristics of the system in flight simulator, and makes clear the data relationship between the virtual aircraft instrument system and other subsystems in flight simulator, including the function request as well as performance request for the system. with professional software vaps design the appearance of virtual aircraft instrument uses atn ( augment transition network model ) to develop the

    通過對整個虛擬航空儀表系統的需求分析，找到作為飛行模擬器虛擬航空儀表系統的自身特點，明確虛擬航空儀表系統和整個飛行模擬器及其它子系統之間的數據關系，結合航空儀表系統的實際應用確定虛擬航空儀表系統的功能要求和性能要求，確定虛擬航空儀表系統開發的整體方案和流程，最終開發整個飛行模擬器虛擬航空儀表系統。
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