飛機系統 的英文怎麼說

中文拼音 [fēijīxìtǒng]
飛機系統 英文
aircraft system
  • 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
  • 系 : 系動詞（打結; 扣） tie; fasten; do up; button up
  • 統 : Ⅰ名詞1 （事物間連續的關系） interconnected system 2 （衣服等的筒狀部分） any tube shaped part of ...
  • 飛機 : airplane; plane; aeroplane; kite; bird; aircraft
  • 系統 : 1. （按一定關系組成的同類事物） system 2. （有條理的;有系統的） systematic
  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. Like the acmi system, nacts is composed of pods carried on aircraft, remote sensors located on the red flag ranges, a host computer and debriefing and display subsystems

    跟acmi系統一樣， nacts由飛機上攜帶的掛艙，分佈在紅旗訓練場中遙感探頭，以及一個進行任務報告和顯示電腦主機系統組成。
  4. Finally, the thesis developed 3d animation flight simulation platform for helicopter using opengl in visual c + +. and the 3d terrain and helicopter model are constructed. the simulation of two typical maneuver ( s maneuver flight and bopup - bopdown ) and terrain following shows that the fight control system of attack helicopter is improved by the realistic optical impact

    本文最後在vc環境下用opengl開發了直升機三維動畫模擬平臺，構造了三維地形和直升機模型，模擬了直升機做蛇形機動、急躍升急躍降、地形跟隨等機動飛行，通過逼真的視覺效果驗證了飛控系統的正確性。
  5. Focusing on the advance research of the flight control computer system of some type of a high altitude, long endurance unmanned aerial vehicles, this paper analyzes and research its staicture in techniques of redundancy fault - tolerance

    本文針對某型號預研高空長航時無人機飛行控制計算機系統的可靠性要求，運用冗餘容錯技術對其進行了設計研究。
  6. Firstly discussing basic type of computer redundant structure and characteristic of the systems, the self - monitoring dual redundancy computer systems is brought forward as the design scheme for the required flight control computer system. the redundant structure is researched about reliability by using markor model and is carefully designed

    首先分析了計算機冗餘結構的基本類型以及本次設計的要求特點，選擇了自監控二冗餘飛行控制計算機系統的設計方案，運用馬爾科夫模型對此冗餘系統的可靠性進行了計算研究，並且對此冗餘結構進行了詳細地描述及設計。
  7. Human reliability analysis and technologies concerned are studied in this thesis, including ergonomics, human error analysis, human reliability analyzing and human reliability evaluation. the collection and analysis of human reliability data are discussed as well, and a database for human reliability is established

    本文圍繞無人作戰飛機系統深入研究了人的可靠性及其相關技術，包括工效分析、人的差錯分析、人的可靠性計算和人的可靠性評估，最後還討論了人的可靠性數據的收集和分析，建立了人的可靠性數據庫。
  8. The total auto symbol recognition disposition method proposed in this paper can deal with the problem which converts papery of aircraft theory graphics or system graphics into vectorgraphs which can lose some useful information. furthermore, the display technique with multi - level buffer not only resolves the problem of high - speed for aircraft theory graphics or system graphics in cbt, but also ensures scrolling and zooming in / out smoothly and avoids the flashing phenomenon efficiently

    目前紙質的飛機系統圖、原理圖矢量化方法用基本的矢量圖元按其位置來再現原始圖，從而導致矢量后圖中各符號整體信息丟失問題，該文提出的自動符號識別方法可有效地解決該問題，此外改進多級緩沖顯示技術不但可有效地解決cbt中系統圖、飛機原理圖的快速顯示，而且也保證圖形可連續光滑滾動和消除放縮拖動時屏幕閃爍現象。
  9. Mr leung explained that reportable occurrences under the mor system include incidents which involve damage to aircraft, injury to person ( including crew ), failure of multiple aircraft systems or equipments, false fire warning and abnormal functioning of communication system

    梁汝強解釋說，在強制事故報告制度下的需作報告事故，包括航機損壞、有人受傷（包括機組人員） 、多重飛機系統或儀器失靈、火警警報誤鳴及通訊系統失常。
  10. In this paper, the method vision - based for uav autonomous landing is researched using technology of image processing, computer vision and projection geometry. the first task of computer vision - based uav autonomous landing is to recognize and track the runway using computer vision. a simple method is discussed to recognize and track the runway in the image sequences using template matching

    本文的研究工作來源於「 973 -無人作戰飛機系統」項目，以某型無人機試飛過程中拍攝的著陸場景圖像為基本研究材料，綜合利用了圖像處理技術、計算機視覺技術、射影幾何學等方法研究了跑道識別與跟蹤、進場著陸段的圖像處理、無人機著陸段飛行參數提取等相關問題。
  11. Work breakdown structures and codes for aircraft systems

    飛機系統工作分解結構及代碼
  12. A survey on ucav system

    無人作戰飛機系統綜述
  13. The second chapter of the paper talks about develops, composes and key problems of ucav system

    本文第二章講述了無人作戰飛機系統的發展、組成及其關鍵技術。
  14. But using the animation pattern to show the airplane ’ s system or circuit principle etc is easy to learn and understand of cbt students

    而用動畫方式來演示飛機系統、電路等原理圖的工作原理是十分易於學員學習和理解。
  15. The reliability of human machine interface system for ucav is evaluated with fuzzy reliability theory. the key effect on human reliability is analyzed

    對無人作戰飛機系統的人的可靠性進行了模糊評估，分析了影響無人機系統人的可靠性的關鍵因素。
  16. If the engine is " heart " of the plane, then the power system is " blood " of the plane, so the importance of power system among the whole plane system is self - evident

    如果說發動機是飛機的「心臟」 ，那麼電源系統就是飛機的「血液」 ，電源系統在飛機系統中的重要不言而喻。
  17. Synthesize to guarantee is the life line of the modem airplane, directly the usage relate toing the right airplane support and the intact rate, training of war preparedness he used as to synthesize the training method that guarantee that one of the important main factors, our method towards customer can on time but accurately control airplane system principle with outfield support function rising key, but now all or many or littlely exsits some blemish, ca n ' t completely attain the anticipant result

    綜合保障是現代飛機的生命線，直接關繫到對飛機的使用維護以及戰備完好率，培訓作為綜合保障的重要要素之一，它對用戶能夠及時而準確地掌握飛機系統原理和外場維護方法起著關鍵的作用，但目前的培訓方式都或多或少地存在某些缺陷，不能完全達到預期的效果。
  18. In the first part, human - machine interface design of ucav ( unmanned combat air vehicle ) is studied. the design criterion of display, controller and working environment for human in ucav system is presented. in the second part, based on the analysis of human error cause, human generic error model is presented

    論文的第一部分研究無人作戰飛機系統的人機界面設計，論文給出了無人作戰飛機系統的功能框圖，根據無人機的任務剖面，綜合功效學的研究成果，給出了無人機系統的顯示裝置、控制裝置、工作環境和操作人員的組織情況等的設計準則。
  19. Stress - strength interference model of structure reliability is introduced to analyze human reliability. the decrease speed of strength with time is studied by the human stress - strength interference model, and its probability density function is derived. similar to engineering reliability analysis method, ucav system reliability diagram and fault tree are presented, fmeca is also performed

    論文的第二部分研究無人作戰飛機系統的可靠性分析，在對人的差錯的原因深入分析的基礎上，建立了人的通用差錯模型，借鑒結構可靠性分析方法，建立了人的可靠性的應力強度模型，推導了強度隨時間下降速率的概率分佈；運用工程可靠性分析方法，建立了無人作戰飛機系統的可靠性框圖、故障樹，並且做了人的差錯的故障模式影響分析。
  20. The nonlinear decoupling method applied on full, hi - fidelity aircraft analysis model was unprecedented, many technique, such as disassemble - design, assemble - apply, multi - grade decoupling, were used so that the nonlinear decoupling method can be used on such a complex model. the successful design of a roll angle and overload decoupling controller show that the nonlinear decoupling is a feasible method for engineering application

    非線性解耦方法在高真實度的完整飛機系統分析模型上的應用在國內尚屬，文中採用分解設計、組合應用、多級解耦控制結構等方法，解決了非線性解耦方法難于應用於復雜系統的問題，成功地設計了滾轉角及過載解耦控制器，達到了較好的控制效果，為工程設計提供了新的途徑。
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