飛行故障 的英文怎麼說

中文拼音 [fēihánggùzhàng]
飛行故障 英文
flight failure
  • 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...
  • 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
  • 飛行 : flight; flying; aviate; voyage; volitate; hop
  • 故障 : hitch; breakdown; stoppage; fault; faulting; accident; blunder; bug; conk; failure; impairment; i...
  1. The airmen were under orders to abort their mission if on-board equipment showed the slightest glitch.

    飛行員事先接到命令，如果機載裝備發生哪怕一點點的故障，也要取消所執行的任務。
  2. 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。
  3. 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。
  4. According to collecting and analyzing the fault information of the jyl - 6 weather radar which is assembled in one of the main planes of the air force, we found the vulnerability on the radar ? design and technics. then we made some correction and the product ? dependability is improved

    本文通過對配裝空軍某重點飛機的jyl - 6氣象雷達研製、生產、使用中的故障信息進行統計、分析，找出該雷達設計、工藝中存在的薄弱環節，加以改進。
  5. In this system, we use a computer model to simulate the true aeromodelling ' s wing, and then we simulate the state of aeromodelling ' s wing under the real flying conditions by computer. moreover, we simulate two fault - models for wing ' s model, and then we get the state ' s date of wing ' s model structure when the two faults are happening

    在建立這個健康監控系統中我們採用在計算機上建立的模型來模擬航模飛機的機翼並在計算機上模擬了飛機在真實情況下的飛行受力狀態，接著我們在計算機上針對機翼模型模擬了二個故障，並計算出了在這二個故障發生時機翼結構的受力狀況。
  6. 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。
  7. At the end of an 18 - hour return trip from manila, as air force one is about to begin its descent into andrews air force base, a cockpit indicator light leads the crew to believe that the landing gear might not be locked down

    空軍一號經過四十八小時飛行，正載著傑克、心靜等白宮幕僚回國，當準備降落安德魯空軍基地之際，機師突然發出著陸裝置故障的訊息，機組人員在飛機於半空盤旋之際進行搶修及檢查。
  8. It is reported that the mechanical failure accounts for most of the aviation accidents, and among them, the wear faults occupy a considerably large proportion rate. based on the traditional ferro - graph and spectral analysis technology, and with the introduction of computer vision and information fusion technology, this article focus on the study of aviation engine abrasion diagnoses in the fields of debris analysis and information fusion

    據統計，導致飛行事故的主要因素是機械故障，其中，磨損類故障又占很大比例，本文就以傳統的鐵譜分析技術和光譜分析技術為基礎，引入計算機視覺與信息融合技術，開展基於磨粒分析和信息融合的航空發動機磨損故障診斷技術研究。
  9. One of the plane 's engines gave out in mid-atlantic.

    飛機在大西洋中部飛行時，其中一個發動機出了故障。
  10. A sudden engine failure forced the pilot to ditch ( in the irish sea )

    由於發動機突然出現故障，飛行員不得不（在愛爾蘭海上）緊急降落
  11. According to the fault type of the flight control surfaces, they are classified and modeled

    文中對飛機操縱面可能出現的故障進行分類，建立數學模型。
  12. His neighbor always let his chickens loose, and they ran over to reach the garden to dig out the roots and eat the flowers and make a mess everywhere. and he told his neighbor to keep the hens within his fence. but the neighbor said, " i don t believe in this kind of restriction, imprisonment

    有一架飛機發生故障，飛行員就用無線電向機場塔臺求救：呼叫塔臺，呼叫塔臺，緊急求救，緊急求救，我離陸地有300英里，離水面有600英尺，飛機快沒油了，引擎著火，儀錶板也出問題了，副駕駛又心臟病發，請趕快指示我該怎麼辦？
  13. Since hale uav has a feature of high altitude and long endurance, the probability of control surface failures is increased highly. when it does happen, the failure would most likely result in fatal accidents

    由於它飛行高度高、續航時間長，使得執行任務期間飛行控制系統出現故障的概率大大增加，這類系統一旦發生事故就會造成巨大損失。
  14. First, a great deal of aerodynamics and moment parameters are processed by look - up table, and then the flight simulation model of normal aircraft and fault aircraft are established

    首先，利用look - uptable對大量的氣動力參數及氣動力矩參數數據進行了插值處理，並在此基礎上建立了正常和故障飛機飛行的模擬模型。
  15. A flight simulation system of the normal aircraft and fault aircraft self - repairing is established by matlab programs based on a robust adaptive tracking control method which is presented according to the fuzzy t - s model

    本文在matlab語言環境下建立了基於t - s模糊模型和自適應神經網路跟蹤控制律的正常飛機與故障飛機自修復的飛行模擬系統。
  16. 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。
  17. 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。
  18. 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
  19. From the spring of 1942 until the war ended in august 1945, pilots ' skills were tested as they crossed towering mountains in abysmal circumstances ? violent turbulence, japanese airfire, dreadful weather, malfunctioning airplanes ? and with little sleep

    從1942年春直到1945年8月戰爭結束，崇山峻嶺及險象環生的環境中? ?強勁氣流、日軍炮火、惡劣天氣、飛機故障? ?飛行員們忍受著睡眠不足，一次次的接受考驗。
  20. The idea of on - line compensating with neural network is introduced to eliminate the inversion error which resulted from the inaccurate fighter ' s model and the faults of the fighter. the dynamic performance is improved by the weight value ' s adaptive adjust of the neural network

    為了消除由於模型不精確和飛行故障等所引起的求逆誤差，設計自適應在線神經網路用於補償非線性動態逆誤差，根據神經網路權值的在線調整來提高系統的動態性能。
分享友人
分享到 Line

分享到臉書