飛行系統 的英文怎麼說

中文拼音 [fēihángxìtǒng]
飛行系統 英文
flight 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...
  • 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...
  • 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 ...
  • 飛行 : flight; flying; aviate; voyage; volitate; hop
  • 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. Flight control system ( fcs ) sensor is used for measuring various kinds of mobile parameters of aerocraft, describing its mobile state and spacial position. it is the principal subunit in the fcs

    飛控系統傳感器用於測量飛行器的各種運動參數，描述飛行器的運動狀態及其在空間的位置，是飛行控制系統的首要環節。
  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. Provision of electronic flight strip trial system

    提供飛行進程單電腦化試行系統
  4. To facilitate technical and operational evaluations of new electronic flight strip system at hong kong international airport

    為香港國際機場引進全新的飛行進程單電腦化試行系統以作技術和操作評估
  5. Numerical simulation of air sliders in an ultra sub - micron flying system

    深亞微米飛行系統滑塊的數值模擬
  6. By the means of integration of theory with practice, the way how the dangerous weather factors affect the flight safety and the way to deal with have also been analyzed. at last, this thesis analyzed the flight accident at wuhan on 22nd, june, 2000. with synoptic chart, code, satellite nephogram, and radar chart, this thesis explained how the dangerous weather affects the aviation flight safety

    文章最後，採用系統分析方法，對2000年6月22日武漢空難事故產生的天氣因素進行了綜合分析，通過對事故發生期間的天氣圖、電碼、衛星雲圖和雷達圖進行系統分析，指出了造成這次事故存在的危險天氣種類，它們的演變過程，對飛行安全的影響。
  7. So the aviation has installed the ground proximity warning system ( gpws ) on aircrafts since the middle of 1970s, and now is the enhance ground proximity warning system ( egpws ). this paper describes the development, components, principle and the features of the communication navigation surveillance / air traffic management ( cns / atm ), the traffic alert and collision avoidance system ( tcas ), ground proximity warning system ( gpws ), and / or the enhance ground proximity warning system ( egpws ). it particularly discuses the positive effect that ads tcas / tcas2 and gpws / egpws take on cfit and middle _ air collision. integrating with the aircrafts type. the instances and the accidents. this paper analyzes the present problems in the field of air traffic management and the new technologies resolving these problems. so that we can improve the flight safety effectively

    本文論述了新航行系統（ cns atm ） 、空中交通警戒與防撞系統（ tcas tcas2 ）以及近地警告系統（ gpws ）和增強型近地警告系統（ egpws ）的發展、組成原理及其功能特點，著重討論了自動相關監視（ ads ） 、 tcas tcas2和gpws egpws在保證飛行安全、防止空中相撞和可控飛行撞地事故中所起的積極作用，並結合具體機型和事故事例，分析了事故發生的原因和目前存在的問題，對系統提出了進一步改進的可能，以期進一步保證飛行安全。
  8. 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。
  9. The system hardwire includes : flexible vehicle management system architectures, fiber optic cable plants, active hand controllers, primary flight control computers, optical mechanizations and smart actuators

    同時還介紹了一單通道主飛控系統的地面演示和一副翼配平控制系統的飛行演示。
  10. The final report, " architecture and evaluation of a formation flight system for existing cargo aircraft, " was submitted for publication and is cited below

    最後一篇報告「以現有貨機來編隊飛行的建構和評估」 ，詳細的研究是根據以下的連結「編隊飛行系統提案的參考資料」 。
  11. The flight ' s atmospheric dynamic characteristics is considered, the aircraft is modeled as a combination of objects. most compositions, such as scene system, flight system, flight ' s sound and control surface are all simulated

    ）等建模軟體建立了相應的三維表現模型；模擬了飛機的主要系統：飛行系統、視景系統、儀表系統和音響系統。
  12. A integrated flight / propulsion control ( ifpc ) theoretical schema was designed based on this concept and a engineering schema was developed after take consideration of currently engineering condition and the requirements of in - service aircraft upgrade. a auto - flight system was designed which can achieve accurate flight movement control and increase performance of flight task such as ascend, cruise, te

    基於該概念設計了飛推綜合原理方案，並在考慮工程實現條件及現役飛機改進、改型要求后建立了工程實現方案，設計了軌跡跟蹤方式的自動飛行系統，解決了軌跡生成、表示、管理、跟蹤等問題，能夠實現運動狀態的精確控制，提高爬升、巡航等任務的性能。
  13. As to the modelling of integrated flight / propulsion system, this paper mainly investigated and the modelling methods of flight kinetics and propulsion system thermodynamics, building up the real - time models of body kinetics. then we integrated the component - level thermodynamics model of engine, solved the problem of matching of initial points in the integrated simulation of flight / engine and the interactive parts of flight system and propulsion system

    對于綜合飛行/推進系統建模，本文主要研究的是飛行動力學和推進系統熱力學的建模方法，建立了飛機動力學實時模擬模型。並結合前人已建立的發動機部件級熱力學模型，本課題在解決了飛機/發動機綜合模擬中的起始點匹配問題的基礎上，完成飛行系統和推進系統的交互部分，最終建立飛行/發動機綜合實時模擬模型。
  14. The aim of this thesis is to analyze the panel flutter mechanism and establish a mechanical model for panel flutter analysis and this work is the basis of panel flutter control studies

    本文的目的就是對壁板的熱顫振特性進行系統深入的分析和研究，為高速飛行器的壁板結構的防顫振設計和壁板顫振抑制的研究建立理論基礎。
  15. Design and development of 3d terrain flying system based on geolod

    軟體平臺下的三維地形模擬飛行系統的設計與實現
  16. 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。
  17. The fast development of computer science and electron technology make the appearance of virtual aircraft instrument system that highly integrates the digital information from airborne devices possible and the cockpit layout could be easily changed while the pilot can get flight information more quickly and control the aircraft more efficiently

    計算機技術以及相應電子技術的高速發展，以及高度集成機載電子設備信息的多功能虛擬儀表系統出現，改變了以往飛機座艙中儀器儀表紛繁復雜的布局，使得飛行員能快速獲得飛行信息，從而更加有效地操縱和管理整個飛行系統。
  18. So almost all airline ads are going to be about how comfortable and pleasant it is to fly and how pampered you will be every step of the way

    舉例來說，飛機旅行又擠又不舒服，空服員無禮又討人厭，其實整個商務飛行系統就是拿來折磨人的。
  19. Part two is the comparison of route system, airport, aircraft and self - service with the traditional airlines to analyze the contribution of these operation decisions

    2 、分析美國西南航空的點對點飛行系統、二線機場、單一機型和簡單自助服務與傳統航空公司飛行系統和服務的不同，對于降低成本的作用。
  20. Secondly, software engineering method is introduced to the course of deve - lopment of the platform, which is intended to solve some common problem occurred in development of flight control simulation system and standardize the process of analysis and coding

    該控制功能框架實現了建模框架和模擬框架的分離。其次，針對飛行模擬系統開發中存在的問題，通過對飛行系統模型及模擬系統的具體分析，引入軟體工程方法。
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