飛行要求 的英文怎麼說

中文拼音 [fēihángyāoqiú]
飛行要求 英文
operational requirements
  • 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...
  • 要 : 要動詞1. （求） demand; ask2. （強迫; 威脅） force; coerceⅡ名詞（姓氏） a surname
  • 求 : Ⅰ動詞1 （請求; 要求） ask; beg; request; entreat; beseech : 求人幫忙 ask sb a favour; ask a favou...
  • 飛行 : flight; flying; aviate; voyage; volitate; hop
  • 要求 : ask; demand; require; claim; requisition
  1. No. 3 good mobility, advertising aeroboat can fly on compeition field, plaza or the sky on a car race, or fly according to the customer s requirement in the sky above the seashore, village, road or city, the advantages can not be all presented by any other media

    三：移動性能好，廣告飛艇既能在賽場，廣場，賽車場上空定點飛行，也可根據客戶要求在海濱，鄉村，公路及城市上空移動飛行，這些優勢是其他戶外媒體所不能同時具備的。
  2. In nineteen seventeen, blacks who requested acceptance into pilot training programs were told that colored air groups were not being formed at the time

    1917年，要求接受參與飛行員培訓項目的黑人被告知那個時候有色種族的飛行隊還不能建立。
  3. Since the earliest man-powered flights, airframe design has demanded an ever-improving standard of technology.

    從最早的人力飛行以來，飛機機體的設計要求不斷地改進工藝質量標準。
  4. Because it ’ s hard to get radiation - harden hardware overseas, so the software fault tolerance techniques are significant for our national space enterprise. the computer platform of 863 plan project ” micro intelligent free - flying space robotic system ” consists of cots component. the orbit and the radiation environment of the robot are similar to ones of the argos satellite, and the system is required to have high reliability. therefore it ’ s necessary to applied the software fault tolerance techniques into the system to improve the anti - radiation capability after the techniques been verified valid

    因為我國很難從國外獲得輻射加固的硬體，所以，這項軟體容錯技術對我國航天事業的發展具有較大意義。 863計劃項目「小型智能飛行機器人系統」所用的計算機平臺採用商用器件，其衛星的運行軌道與argos衛星軌道近似，面臨的輻射環境與argos衛星相似，要求具有高可靠性。因此，小型智能飛行機器人系統有必要在驗證sihft技術有效的基礎上，應用軟體容錯技術，提高其空間抗輻射能力。
  5. Aircraft ground support equipment - specific requirements - part 6 : deicers and deicing antiicing equipment ; german version en 12312 - 6 : 2004

    飛行器地面支持設備.特殊要求.第6部分:去冰機和除冰
  6. He asked them to discontinue flights over the island.

    他要求他們停止在該島上空飛行。
  7. In the case of aircraft operating at 26, 000 to 49, 000 all of the cathay pacific airways fleet, euratom requires that the dosage to crew members should be assessed by computer program prediction

    對于在二萬六千尺至四萬九千尺高空飛行的航機包括所有國泰飛機， euratom要求電腦程式推算機組人員的輻照量。
  8. Euratom requires that that aircraft capable of operating at altitudes of more than 49, 000 feet should be equipped with active radiation monitors. cathay pacific airways does not currently have any aircraft of this type

    Euratom要求在四萬九千尺以上飛行的飛機安裝活躍輻射監測儀，國泰航空目前並無此類飛機。
  9. Airplane flight simulator standards

    飛機飛行模擬機等級要求
  10. The design point of the designed forebody / inlet is flight mach number m = 6 and flight attitude h = 25km. the three - ramp, mixed external and internal compression hypersonic / inlet is chosen as representative geometry to be designed. nine types of hypersonic / inlet model with difference forebody length and total turning angle are obtained that the incidence angle of the first ramp and height of isolator are given

    根據飛行任務要求，以飛行馬赫數6 ，飛行高度25km為設計點，給定前體預壓縮角、隔離段高度，對具有不同前體長度和不同總壓縮轉角的帶隔離段的前體進氣道進行了設計。
  11. On the basis of introducing the principle of the tf / ar radar, this paper analyzes the conditions of effectively jamming the tf / ar radar in typical tactical act of hedgehopping, which include the disposition and quantity of electron reconnaissance / jammer, calculates the capability request of equipments in the method of sensor / hand - emplaced jammer, and concludes that it is difficult to jam tf / ar radar at the present time

    摘要在介紹地形跟隨迴避雷達工作原理的基礎上，通過設定典型超低空突防飛機的戰術行動，分析了對雷達實施有效干擾所必須具備的條件，包括偵察干擾機的部署、數量要求等；並計算了在傳感器擺放（投擲）式干擾機模式下對裝備的性能要求，得出了在目前技術條件下，對地形跟隨迴避雷達實施干擾在技術和戰術上都是困難的。
  12. The method of wing shape optimization of space shutlle has been developed with penalty function approach in which the objective function is the mass of the wing and the constraints are the hypersonic re - entry flight cross range, lift / drag ratio, and subsonic flight lift / drag ratio, the margin of the longitudial static stability and the magnitude of the horizontal landing speed etc

    摘要介紹了在滿足高超音速再入橫向機動航程，高超音速再入飛行時的升阻比，亞音速進場飛行時的升阻比，縱向靜穩定性裕度和水平著陸速度等飛行性能設計要求下，用罰函數法尋求使航天飛機機翼質量為最小的外形優化方法並給出了算例。
  13. Aircraft ground equipment - lower deck loader - functional requirements

    飛行器地面設備.底艙板裝載機.功能要求
  14. It sets higher demands for the pilots and machinists

    這就對飛行員和機械師提出了更高的要求。
  15. In comparison to other flying objects, it features low altitude, low flying speed, stable, safty, easy operation, low cost, specially suitable for video taking by air, geo - measuring, it is the best choice for news, moviedom, mapping ect.

    熱氣球與其他飛行器相比，其低空低速平穩安全操控簡單飛行成本低廉等特點特別適合於空中攝影攝像地形測量等的作業要求，是新聞影視測繪等行業的最佳選擇。
  16. In this paper, some flows around naca 0012 aerofoil, m6 wing and two different blunt vehicles are simulated, the results show that the present algorithm possesses good characteristics and capability for normal mach number and for hypersonic of simple configurations

    通過對naca0012翼型、 m6機翼、鈍頭以及雙鈍錐?柱體的算例驗證，本文能很好的解決一般馬赫數問題，能夠很好的求解簡單外形的高超聲速問題，對于復雜外形飛行器還需要進一步進行研究驗證。
  17. The linear scaling and the reynolds number represent classical, aerodynamic similitude requirements applicable to law-speed flight.

    線性縮尺和雷諾數是低速飛行時經典的氣動力模似要求。
  18. Aircraft structural integrity program, airplane requirements

    飛行器結構完整性大綱.飛機要求
  19. Abstract : the control reconfigurable aircraft with multi - surfaces needs robust basic flight control system to support enough time for failure detection and isolation. when partial surface loses, it can keep the damaged aircraft stable. in this paper, multivariable output feedback digital control laws are designed for the control reconfigurable aircraft ( cra ). the method uses fast - sampling digital pi controllers to design digital flight control tracking system. this paper gives the way to design the controller and analyze its robustness characteristics. the simulation results indicate that the controller is very robust and the output responses are fully satisfactory

    文摘:控制可重構飛機要求其基本飛行控制系統對舵面部分缺損故障具有強的魯棒特性，在故障發生后保證飛機的穩定性，提供足夠的時間進行故障的檢測和隔離，為控制系統重構提供條件.本文採用高速采樣pi控制器設計輸出反饋跟隨系統，給出了控制器的設計方法，並分析了它對于控制舵面部分缺損故障的魯棒特性.模擬結果表明，這種控制器具有好的魯棒特性
  20. Generally speaking, the algorithm of terrain contour matching is adapted to be used in cruise missiles which made fight path prior for that this algorithm is not a real - time system for it makes use of historical terrain data. while kalman filter algorithm is a real - time, rapid calculation system. which is appropriate for pilot or pilotless aircraft

    得出，地形輪廓匹配演算法使用歷史地形數據，實時性差，比較適合事先規劃好航跡的導彈使用：卡爾曼濾波的方法有較好的實時性，計算速度快，很適合有人無人駕駛飛機的機動飛行要求；小波分層只是對地形信息做了高低頻分解，其本質還是相似性度量演算法，但它有效的降低了匹配演算法的計算量。
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