舵力特性 的英文怎麼說

中文拼音 [duòxìng]
舵力特性 英文
rudder force characteristic
  • : 名詞(船、飛機等控制方向的裝置) rudder; helm
  • : Ⅰ名1 (力量; 能力) power; strength; ability; capacity 2 [物理學] (改變物體運動狀態的作用) forc...
  • : Ⅰ形容詞(特殊; 超出一般) particular; special; exceptional; unusual Ⅱ副詞1 (特別) especially; v...
  • : Ⅰ名詞1 (性格) nature; character; disposition 2 (性能; 性質) property; quality 3 (性別) sex ...
  • 特性 : characteristic(s); character; performance; features; properties; behaviour; response; character...
  1. The structure and principle of two different types of ema are systematically presented. the load characteristics and mechanical characteristics are analyzed with emphasis on the influence of the hinge torque on their dynamics and static characteristics

    系統描述了兩種不同類型的電動機的結構、工作原理,分析了其負載及機械,並著重討論了鉸鏈矩對機動、靜態的影響。
  2. It is difficult to replicate hinge moment accurately and rapidly because surplus torque affect dynamic performances of load simulator system badly with large intensity and continuous variation derived from variable velocity of rudder system

    這種干擾作用具有強度大、隨機速度不同連續變化的點,它的存在嚴重影響了負載模擬器的動態能,使得加載系統難以準確、快速地復現空氣動鉸鏈矩。
  3. In this paper, the backward simulation was summarizd at home andabroad, the characteristics of shell nosing were introduced, the theory and scheme of backward simul - ation of shell nosing was constructed, the determined methods of the boundary conditions were put forward in backward simulation for the processes of shell nosing

    論述了推矢量控制技術是提高空空導彈能的核心技術,介紹了常用的三類推矢量裝置,著重討論了燃氣式和擾流片式推矢裝置的點、設計方法、能及其優缺點.在此基礎上,研究了適用於氣動/推矢量復合控制的變結構控制系統及其開關函數的切換條件和飛行控制系統框圖.最後綜述了推矢量裝置在第四代空空導彈上的應用情況
  4. Secondly, the dynamic features, surplus torque and loading gradient features of ptss are analyzed by the couple model between the rudder and the eals. it can be concluded that the surplus torque is related directly to the velocity of the rudder, and the loading gradient is the disturbing inverse ratio from the surplus torque to the closed - loop model, which shows the scaling relationship between the input and the disturbance signal act on the eals. it also can be concluded that, under the same dynamic specification, it is more difficult to realize the small loading gradient

    然後,採取把系統模型轉化為機和負載模擬器相互耦合作用的形式,對被動式矩伺服系統動態、多餘矩和加載梯度一一進行理論分析,得出:多餘矩與機運動速度直接相關;加載梯度是在系統閉環模型中,與多餘矩相關部分模型幅值大小成反比的系數,體現了被動式矩伺服系統的指令信號和擾動信號之間的比值關系,從而在相同的動態指標下,小加載梯度實現更為困難。
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