有故障的飛機 的英文怎麼說

中文拼音 [yǒugùzhàngdefēijī]
有故障的飛機 英文
ailing aircraft
  • 有 : 有副詞[書面語] （表示整數之外再加零數）: 30 有 5 thirty-five; 10 有 5年 fifteen years
  • 故 : Ⅰ名詞1 （事故） event; incident; happening; accident 2 （原因） cause; reason 3 （朋友; 友情） fr...
  • 障 : Ⅰ動詞（阻隔; 遮擋） block; hinder; obstruct Ⅱ名詞（遮擋物） barrier; block; obstacle
  • 的 : 4次方是 The fourth power of 2 is direction
  • 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...
  • 機 : machineengine
  • 故障 : hitch; breakdown; stoppage; fault; faulting; accident; blunder; bug; conk; failure; impairment; i...
  • 飛機 : airplane; plane; aeroplane; kite; bird; aircraft
  1. Recordings from the cvfdr gave no indication of any aircraft system failures during the flight and no emergency call was made by the crew. neither air traffic control nor the gfs received any distress call from the helicopter

    記錄儀並沒有錄得直升機系統故障，機組人員也沒有發出緊急呼號。航空交通管制和政府飛行服務隊均沒有收到由肇事直升機發出的遇險呼號。
  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. The approaching aircraft was an airbus a320 which had departed hong kong for phnom penh but returning due to a minor electrical problem. as the aircraft was number one in the approach sequence, it was allowed to fly at its own speed

    該進場飛機是一班從香港飛往金邊的空中巴士a320 ，因電力系統有輕微故障而須折回，因這航機是第一班進場的飛機，所以讓飛行員保持其進場速度。
  4. Finally, a fault diagnosis system of civil aircraft was developed on the jade platform, and realized the distributed cooperation diagnosis of many cbr - agents based on contract network, as the combination of the cbr method and the agent technology, the system has the properties of collective intelligence, good robustness and better fault tolerance

    最後，在jade平臺上實現了採用合同網方式的多個cbragent分散式協作診斷，開發完成了民用飛機故障診斷系統， cbr推理方法及agent技術相結合的使用，使得該系統具有集體的智能性、較好的健壯性與容錯性。
  5. The objective of this thesis is to design an artificial neural network adaptive reconfigurable flight control law basing on the view of engineering and to establish a flight simulation system with normal aircraft, fault aircraft, normal flight control law, reconfigurable flight control law and fault verification by c + + program

    本文目的是從工程角度考慮，重點開發神經網路自適應的自修復重構飛行控制律。並在c + +環境下建立具有正常與故障飛機、正常與自修復重構飛行控制律和故障認定等模塊的飛行綜合模擬系統。
  6. Using this model, not only the normal static and dynamic characters of aircraft epgs but also the fault state system can be simulated. it is useful to analyse and design aircraft epgs

    利用本文開發的模型，不僅能模擬電源系統及其部件正常工作時的穩態和動態特性，而且能模擬其故障狀態，有助於對飛機電源系統進行分析和設計。
  7. This dissertation investigates design of reconfigurable flight control systems of a certain model hale uav which is supported by initiative research project fund of china during the 10th 5 year plan

    本文以我國某型高空長航時無人機預研項目為背景，設計具有高生存力的可重構飛行控制系統，實現單一故障條件下飛機的可靠正常飛行。
  8. 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
  9. Nowadays, in the process of airplane maintenance, when airplanes are towed to move on the parking apron or in the garage, they are often on the hazard of bumping with the garage wall or other barriers at the dangerous points ( such as head, wings or tail ) because of their bulkiness. but the maintainers have to avoid these accidents by eyes

    目前，在飛機保養與維修過程中，由於飛機體積龐大，飛機在停機坪上或機庫中被拖拽做地面移動時，機翼、機頭、機尾等危險點，經常有可能與機庫墻壁或其他障礙物碰撞，而維修人員只能靠目測來防止此類事故的發生。
  10. In modern aviation technology, although there is fine oxygen system, pilots often suffer from different hypoxia because of loss of cabin pressure, unfitness of mask, trouble with oxygen system, and so on

    在現代航空中，雖然有良好的供氧防護裝備，但由於飛機密封增壓座艙失密封、面具佩戴不嚴或供氧系統故障等，均可引起飛行人員不同程度的缺氧。
  11. Since the western countries began the srfcs research in the eighties, theory of signal detection is used in fdi, and it was successful in some fdi functions in several types of testing aircraft. china did the srfcs research recently, but lack of the engineering fdi algorithm. because the " model based signal detection algorithm " is sensitive to the matching accuracy of the mathematics model and aircraft has prominent nonlinear aerodynamic factors, it is difficulty to upgrade the ability of fdi based on the classical signal detection theory and data fusion only

    國外自八十年代開展自修復研究，一般採用基於常規數據處理的故障檢測理論來實現飛控系統故障檢測與隔離功能，現已在幾種驗證機上取得初步成果，而國內的研究尚缺乏實用的工程演算法；同時，基於常規數據處理的故障檢測精度對被檢測對象的數學模型匹配度敏感，且飛機的氣動特性在故障情況下又具有較強的非線性特性，因此，單純依靠常規的信號處理演算法難以進一步提高故障檢測的精度。
  12. In 1997, an explosion of undetermined origin killed a passenger who was blown out of a tam fokker 100 during flight. in 2001 an engine breakup on a tam fokker 100 caused two cabin windows to shatter and one of 82 passengers aboard died as a result of the depressurization

    2001年，還是tam公司旗下的一架載有82名乘客的福克爾100飛機因發動機故障致使兩塊機艙窗戶的玻璃破碎，致使一名乘客因艙內氣壓下降而死亡。
  13. In 2001 an engine breakup on a tam fokker 100 caused two cabin windows to shatter and one of 82 passengers aboard died as a result of the depressurization

    2001年，還是tam公司旗下的一架載有82名乘客的福克爾100飛機因發動機故障致使兩塊機艙窗戶的玻璃破碎，致使一名乘客因艙內氣壓下降而死亡。
  14. In this thesis, on the basis of federated kalman filtering theory and aiming at a certain type of airplane equipped with many navigation equipments such as sins, gps, etc., an integrated navigation system with the fault tolerance property is designed. the thesis is stressed to investigate some new theories and methods of fdi in designing the fault tolerance integrated navigation system

    本論文以carlson提出的聯邦濾波方法作為理論基礎，針對某型飛機裝備的sins 、 gps等多種導航設備設計了具有容錯性能的聯邦濾波組合導航系統，並且在以往三屆研究生論文的研究工作基礎上，著重研究了組合導航設計中有關故障檢測方面的新理論和新方法。
  15. The content includes the study on the fatigue performance of the plexiglas, the compiling of the load spectrum of the canopy, the study on the evaluation of the fatigue life of the canopy glass, the study on the allowable limit of the scratch on the canopy glass and the study on the analysis method of the dynamic response of the bird impact on the aircraft windshield

    所涉及的內容包括:有機玻璃疲勞性能研究、活動艙蓋載荷譜編制、座艙玻璃疲勞壽命估算方法研究、座艙玻璃劃傷故障容限研究、飛機風擋鳥撞動響應分析方法研究等。根據活動艙蓋載荷特性，提出用壓力傳感器測量活動艙蓋載荷的方法，並首次實現了活動艙蓋載荷譜飛行測量。
  16. Referring to the newest proposal on aircraft maintenance of the military of u. s. a and aimming at the problems of the information management system of traditional civil aviation maintainence engineering, this thesis came up with a new system - digital integrated maintenance and support information system ( dimsis ), which is made up by the technologies of computer network, database, communication engineering, software engineering and etc. after its building, most of the requirements of the domestic airlines on information technologies will be met

    該系統將計算機網路、數據庫、通信工程、軟體工程等技術有機結合，首先用internet intranet技術構建企業局域網，然後將飛機維修最原始的資料? ?維修手冊電子化錄入到主機系統，達到在各終端的快速信息訪問，並針對停機坪維修的特點，將有線網進行延伸，在機場搭建基於無線局域網技術的便攜式飛機維護助手pma ，提高飛機的故障排除速度與派遣放行率。
  17. In order to ensure the stable work of fighter planes while increasing their maneuverability, it is necessary to investigate the vibration performance of aero - engine in maneuver flight

    為了確保飛機在提高其機動性能的同時還能穩定工作，不發生故障，有必要對機動飛行條件下的發動機轉子系統的振動特性進行研究。
分享友人
分享到 Line

分享到臉書