推力矢量控制 的英文怎麼說

中文拼音 [tuīshǐliángkòngzhì]
推力矢量控制 英文
thrust vector control
  • : 動詞1 (向外用力使物體移動) push; shove 2 (磨或碾) turn a mill or grindstone; grind 3 (剪或削...
  • : 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名詞1. (箭) arrow 2. (尿) excrement; dung; feces 3. (姓氏) a surname Ⅱ動詞(發誓) vow; swear
  • : 量動1. (度量) measure 2. (估量) estimate; size up
  • : 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...
  • : 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...
  • 推力 : visatergo; soot; propulsive force; thrust; momentum thrust
  • 控制 : control; dominate; regulate; govern; manage; check; cybernate; manipulate; encraty; rule; rein; c...
  1. Deere k a. computational investigation of the aerodynamic effects on fluidic thrust vectoring. aiaa 2000 - 3598

    喬渭陽,蔡元虎.基於次流噴射噴管的實驗及數值研究.航空動學報, 2001 , 16 ( 3 )
  2. A set of non - linear differential equation of this model is formulated based on lagrange ’ s equation. the tension of the cable, the control force of translation and the control torque of rotation are obtained by the method of newton ’ s laws in vector space. the tethered mass system is modeled as a spherical pendulum

    本文基於一種常見的繩系單體系統,運用lagrange方程建立了該系統的非線性運動微分方程,採用法對該運動微分方程進行了校核,並導出吊索的張、變幅和回轉
  3. The application of thrust vectoring control technology makes the aircraft possess the ability to fly in post - stall domain, therefore the flight envelope is extended

    推力矢量控制技術在戰斗機上的應用,使戰斗機有能進入過失速飛行領域,使飛機的飛行包線得以擴展。
  4. The application background of thrust vectoring technology on aircraft and its advantages are analyzed. the main characteristics of some type of vectoring nozzles are discussed, the expression of thrust vectoring force and moment are set up. then, the nonlinear motion equations of aircraft with three axes of thrust vectoring are deduced

    本文主要針對飛機非線性飛行的理論和應用問題進行了一定的探索和研究,進行的主要工作有: 1 、研究了在飛機上的應用背景和收益,分析了現有噴管的主要形式和特點,給出了矩的數學模型,並在此基礎上導了帶三軸飛機的非線性運動方程,為律的設計奠定基礎。
  5. The essay suggested coupling approaches of ecological economic system pointedly with theory of coupling catalyzing and management accesses based on analyzing causes of ecological - economic system coupling status of zhijin county : 1 ) put population into practice with controlling the quantity of population and developing the quality of population ; 2 ) carry out the strategy of revitalizing zhijin through science and education ; 3 ) take ecological - economic management and optimize industrial structure and develop zhijin ’ s economy ; 4 ) protect environment & resources and control karst rocky desertification integratedly ; 5 ) facilitate urban - rural coupling and sustainable development depended on urbanizing

    在原因分析的基礎上,以催化和管理耦合理論為指導,論文有的放地提出生態經濟系統的耦合途徑: 1 )實施人口政策,人口數,提高人口素質; 2 )大實施「科教興織」戰略; 3 )行生態經濟管理,優化產業結構,發展織金經濟; 4 )保護環境和資源,綜合防治石漠化; 5 )以城鎮化為載體,進城鄉耦合和可持續發展。
  6. Using this method, the flight control law which suits to the vectored aircraft flight in post - stall domain is designed in this paper

    運用這種方法對飛機進行了適用於過失速機動的非線性飛行系統設計。
  7. The thrust vectoring control technology and post - stall maneuverability enhance the aircraft ' s combat effectiveness greatly, and cause the worldwide interest

    推力矢量控制技術和過失速機動使戰斗機的空戰效能大大增加,引起了世界各國的關注。
  8. The results show that there are no un - receptible responses when the post stall maneuver modes are applied, and agility is raised significantly

    試驗結果表明,使用的4種過失速機動模式沒有不可接受的操縱響應,飛機採用推力矢量控制后敏捷性明顯提高。
  9. The results show that the control law can control vectored aircraft to accomplish post - stall maneuvers very well and it is very robust to model uncertainty. 4

    模擬結果表明,該律能飛機順利完成過失速機動,對系統模型的不確定性具有較強的魯棒性。
  10. For researching the flight test techniques of thrust vector controlled aircraft, dynamic models of thrust vector controlled aircraft were established, four post stall maneuver control laws were designed with the dynamic inverse method, tested and investigated according to a standard evaluation maneuver set ( stems )

    摘要為研究飛機的試飛技術,建立了飛機的動學模型,用動態逆方法設計了4種過失速機動律,並在地面飛行模擬器上參考標準評估機動動作集( stems )進行了飛行模擬試驗研究。
  11. Here, the aircraft is in extreme flight conditions that is high angles of attack and high angular rates. it can encounter severe nonlinear effects. detailed descriptions of the flight dynamic, aerodynamic models, inverse dynamic and the choice of the control variable are given

    2 、應用經典的微分幾何方法研究了一般的飛行狀態下飛機飛行的律,指出不利用的飛行系統的方程一般都是可以逐步通過動態狀態反饋,適當的坐標變換和正則靜態反饋等三個步驟得以線性化。
  12. 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

    論述了推力矢量控制技術是提高空空導彈性能的核心技術,介紹了常用的三類裝置,著重討論了燃氣舵式和擾流片式裝置的特點、設計方法、性能及其優缺點.在此基礎上,研究了適用於氣動/復合的變結構系統及其開關函數的切換條件和飛行系統框圖.最後綜述了裝置在第四代空空導彈上的應用情況
  13. Thrust vector control

    推力矢量控制
  14. Using the optimal control theory an optimal control law of agile turn is proposed enabling to eliminate velocity component in vertical director of initial sight under thrust vector control

    應用最優理論,提出一種最佳快速轉彎律,能在推力矢量控制下消除終端時刻垂直於初始視線方向上的速度分
  15. And establishing the model of the thrust vectoring nozzle is the base for researching thrust vectoring technique and engine performance with vectoring nozzle, especially the integration of flight and propulsion system control ( ifpsc ). so thrust vector modeling is very important and meaningful

    噴管是實現的關鍵部件,建立其數學模型是技術尤其是開展帶噴管的發動機研究以及飛一體化綜合研究的基礎,具有十分重要的意義。
  16. The mechanism of two possible ways of thrust vectoring control : force and moment control are analyzed. the effects of thrust vectoring on aircraft supersonic performance, take - off and landing performance, low speed and high angle of attack performance are studied. the air combat effectiveness of thrust vectoring control and post - stall maneuvers are also analyzed

    5 、分析了的兩種應用方式:的機理,研究了對飛機超音速性能、起降性能、低速大迎角性能的影響,討論了與過失速機動對空戰效能的影響。
  17. In the vector control, both the no - load thrust and the thrust with the different current are calculated, and the end effect influenced by the current magnitude is analyzed

    運行下,分別計算了電機在空載時和在通以不同電流時的由端部效應引起的波動,並且分析了電流大小對端部效應的影響。
  18. The vector trust control is a most effective method to solve this conflict

    推力矢量控制是解決這一矛盾的極其有效的方法。
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