飛行線控 的英文怎麼說

中文拼音 [fēihángxiànkòng]
飛行線控 英文
fbw
  • 飛 : Ⅰ動詞1 （鳥、蟲等在空中活動） fly; flit 2 （利用動力機械在空中行動） fly 3 （在空中飄浮遊動） fly...
  • 行 : 行Ⅰ名詞1 （行列） line; row 2 （排行） seniority among brothers and sisters:你行幾? 我行三。where...
  • 線 : 名詞1 （用絲、棉、金屬等製成的細長的東西） thread; string; wire 2 [數學] （一個點任意移動所構成的...
  • 控 : 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...
  • 飛行 : flight; flying; aviate; voyage; volitate; hop
  1. That the antenna points at the aerocraft very precisely can utilize the gain of antenna, minishing the power of transmitter, and propagating data very gualitily effectly

    在無線測控系統中，天線精確指向飛行目標，可最佳利用天線增益，減小發射功率，高質量的進行控制和數據傳輸。
  2. 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。
  3. Sufficient or not of the battery on the device should be carefully examined before every flying, so do the every pole, helm and gemel, whether or not is the receiving antenna drew out of the body and in straight, examine the ground effective distance for remote control without the drawing out the antenna, ensure it nomal in rang of 30 - 50 meters

    1 .仔細檢查測試設備每次飛行前都應該仔細檢查設備電量是否充足，檢查飛機各個拉桿舵角鉸鏈是否正常，接收機天線是否拉出機身並拉直，在不拉出發射機天線的情況下測試地面有效遙控距離，確定30 - 50米內不發生跳舵情況。
  4. From straight and level flight, after the helicopter passes the pilot, execute a 180 degree turn away from the pilot

    先保持水平直線飛行，當直升機通過操控者后，開始執行外側180轉彎的動作（遠離操控者） 。
  5. Starting from straight and level flight after the helicopter passes the pilot, the helicopter is smoothly pulled vertical ( aft cyclic )

    先保持水平直線飛行，當直升機通過操控者后，開始平滑地拉高機頭（打升舵） ，使機頭朝上垂直爬升。
  6. Starting from straight and level flight after the helicopter passes the pilot, the helicopter is smoothly pulled through a loop ( aft cyclic )

    先保持水平直線飛行，當直升機通過操控者后，開始平滑地拉高機頭（打升舵） ，使飛行軌跡成為一個環狀。
  7. The first such machine, a radio - controlled “ fairey queen ” biplane, was catapulted into the air in 1933 and survived two hours of live fire from a british warship

    首架這樣的飛行機是一架由無線電控制的雙翼飛機，且名為「仙境中的女王」 ， 1933年被彈射而飛向天空，並在一艘英國軍艦的炮轟下挺了兩個小時。
  8. This paper analyses the applied characteristic of phase - locked loops ( pll ) for the forward motion compensation technology of lmk aerial survey camera. according to the analysis, a new style pcb is produced. the realization by software for the forward motion compensation is discussed in this paper, which is realized by the ti prduction tms320f240

    在對lmk航空攝影機像移補償控制系統的再設計工作中，本人設計出了新的補償電路線路板，並進行了幾項典型的實驗研究和前向運動補償效果評價，經過外場飛行試驗，進一步證明了該設計的可靠性、可行性、實用性。
  9. This is a flight during which the aeromodel is aerodynamically manoeuvred by control surface ( s ) in attitude, direction and altitude by the pilot on the ground using radio control

    本類系指由地面的運動員通過無線電遙控模型改變飛行姿態、方向和高度的項目。
  10. Got the fostering energetically of four - dimensional company since bell model company established, is it produce many kinds of electronic to develop, the oil move the radio telecontrol model plane, the company possesses the stronger model and develops, designs and processes manufacturing capacity, hold concurrently and design the business of the light - duty aircraft, not having man - machine, drone aircraft etc. at the same time

    貝爾模型公司成立以來得到了四維公司的大力扶植，研製生產出多種電動、油動無線電遙控模型飛機，公司具備較強的模型開發、設計和加工製造能力，同時兼承接設計加工輕型飛行器、無人機、靶機等業務。
  11. 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，使戰斗機有能力進入過失速飛行領域，使飛機的飛行包線得以擴展。
  12. In addition, some problems about engineering applications including the influence of regulating parameter to system control effect and the adaptability of the model following controller in flight envelope are discussed

    此外，文中對控制器中的可調參數對控制效果的影響及最終滑動模態變結構模型跟蹤控制器在飛行包線范圍內的適應性等工程應用問題進行了討論。
  13. With the helicopter flying straight and level after it passes the pilot, make a turn that is greater than 180 degrees, away from the pilot

    先保持水平直線飛行，當直升機通過操控者后，向外側（遠離操控者）執行大於180的轉彎。
  14. With the helicopter flying straight and level after it passes the pilot, make a 270 degree turn away from the pilot, the helicopter will now be pointed directly at the pilot

    先保持水平直線飛行，當直升機通過操控者后，開始執行外側3 / 4水平圓（遠離操控者） ，使機頭朝向操控者。
  15. With the helicopter is flying straight and level inverted after it passes the pilot, make a 270 degree turn away from the pilot, the helicopter will now be pointed directly at the pilot

    先保持倒飛水平直線飛行，當直升機通過操控者后，開始執行外側3 / 4水平圓（遠離操控者） ，使機頭朝向操控者。
  16. Fly straight and level form left to right as the helicopter is just about in front of the pilot, pull back cyclic, adjust the collective to maintain constant altitude and speed and hold the back cyclic as the helicopter completes one ( 1 ) full traveling tumbling back flip to upright

    由左至右保持水平直線飛行，當直升機在操控者的正前方時，將升降舵拉升舵，控制主旋翼的螺距使直升機保持固定的高度及前進速度，向後翻滾一圈完畢。
  17. Fly straight and level from left to right at a moderate speed as the helicopter is just about in front of the pilot, add extra collective momentarily, then simultaneously push forward cyclic, and adjust the collective to maintain constant altitude and speed and hold the forward cyclic until the helicopter completes one ( 1 ) full traveling tumbling front flip to upright

    由左至右保持適當速度的水平直線飛行，當直升機在操控者的正前方時，瞬間加大主旋翼的螺距，同時將升降舵打降舵，控制主旋翼的螺距使直升機保持固定的高度及前進速度，直到直升機向前翻滾一圈完畢。
  18. Fly - by - wire system

    線控飛行控制系統
  19. 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控制律，指出不利用矢量推力的飛行系統的控制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。
  20. The current control approaches are based on frequency domain methods such as pid control which assumes linear time invariant system dynamics. the advantages of these approaches are simplicity and ease of stability and robustness analysis. however, the decrease in performanc e and poor efficiency translates to additional payload and cannot meet the demand of current spacecraft control

    當前飛行器主要的控制方法是基於近似時不變線性系統的頻域分析法（如pid控制） ，這種方法的優點是簡單且易於穩定性和魯棒性分析，但它所達到的低性能和低效率卻轉化成了飛行器控制過程的附加載荷，還遠不夠滿足當前飛行器控制的要求。
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