飛控系統 的英文怎麼說

中文拼音 [fēikòngxìtǒng]
飛控系統 英文
afcs automatic flight control 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...
  • 控 : 動詞1 （告發;控告） accuse; charge 2 （控制） control; dominate 3 （使容器口兒朝下 讓裏面的液體慢...
  • 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 ...
  • 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. Thirdly, in the environment of labview, several kinds of vis used for sensor signal test are designed, including wave generation, time domain measurement, filter disposal, frequency analysis, etc. after that, wavelet analysis in the application of one - dimensional signal de - noise is studied, threshold and translation invariance wavelet de - noise are realized, and wavelet de - noise vi for zero drift signal of the fiber optic gyro in fcs is designed using labview

    接著，在labview環境下開發了多種用於傳感器信號測試的虛擬儀器，具有波形發生、時域測量、濾波處理、頻譜分析等多種功能。隨后，研究了小波分析在一維信號消噪中的應用，實現了labview環境下的閾值法和平移不變量法小波消噪，並利用labview設計了飛控系統中光纖陀螺零漂信號的小波消噪儀。
  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. 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。
  6. Fly - by - wire flight control system

    電傳飛控系統
  7. Self - repairing flight control system ( srfcs ) is a kind of active - and passive failure tolerant control based on the fly - by - wire flight control system, and it is also an important tendency of the future flight control system

    自修復飛行控制系統（ srfcs ： self - repairingflightcontrolsystem ）是在電傳飛控系統基礎上發展起來的一種與主動容錯技術結合的先進飛控系統，也是未來戰斗機飛控系統的重要發展方向。
  8. 3 ) definition of input designer concept for flight control system ( fcs ). a input designer was successfully constructed which can provide a effect almost the same as directly control over aerodynamic control surface through the careful design of inputs of fcs. this input design concept is very important for in - service aircraft upgrade where change of the original pcs is not allowed

    3 ）提出了飛控系統輸入設計概念，並成功地構建了飛控輸入設計器，能夠在不改變原飛控系統條件下有效地提高舵面控制能力，獲得接近直接舵面操縱的性能，對于現役飛機改進、改型中飛機運動自動控制系統的設計具有非常重要的意義。
  9. Then above the typical terrain and under the disturbance the terrain following system is simulated. the result shows the flight control system can withstand the disturbance and track the optimal trajectory

    在典型地形情況下進行地形跟隨模擬，並且為了真實模擬地形跟隨，在控制通道加入風擾動，結果表明該飛控系統能夠很好的抵抗風擾動，緊緊跟隨最優軌跡飛行。
  10. Therefore, aiming at the existent static and dynamic error of fcs sensor, the sensor characteristic compensation subunit is designed in the environment of labview using vi technique. the sensor signal disposal platform is also developed to realize the time domain measurement, frequency domain analysis, long - distance transfer and network release, etc. firstly, the static characteristic and nonlinear error of the sensor are analyzed

    為此，本文針對飛控系統傳感器存在的靜態和動態誤差，利用虛擬儀器技術在labview環境下設計了傳感器性能補償環節，開發了傳感器信號處理平臺，對信號進行時域測量、頻譜分析、小波消噪、遠程傳輸和網路發布等。
  11. The flight control system of attack helicopter and the influence of disturbance during noe flight are studied in this dissertation. and the use of h robust control and dynamic inversion schemes in flight control system are discussed

    本文主要對貼地飛行時武裝直升機的飛行控制系統進行深入的研究和探索，討論了貼地飛行時氣流擾動對直升機系統的影響，研究了h _魯棒控制和動態逆控制在直升機飛控系統中的應用。
  12. Self - repairing flight control system ( srfcs ) is a kind of active and passive failure tolerant control based on the fly - by - ewire flight control system, and it is also an important tendency of the future flight control system

    自修復飛行控制系統（ srfcs ： self - repairingflightcontrolsystem ）是在電傳飛控系統基礎上發展起來的一種與主動容錯技術結合的先進飛控系統，也是未來戰斗機飛控系統的重要發展方向。
  13. Then according to system simulation technology, the overall air - to - ground attack simulation plan is made with the thought of models and layers. after that, the mathematical models of main parts in the simulation are made such as aircraft body, propulsive system, flight control system, fire control system, bomb and air - to - ground missile. on the basis of these mathematical models, using the object - oriented design methodology, a set of air - to - ground attack real - time visual simulation software is developed. this software can be used to aid aircraft design, research of air - to - ground attack tactics and flight training

    本文首先介紹了現代戰爭中空對地攻擊的技術裝備及其特點，計算機模擬技術的發展以及面向對象的軟體設計思想；而後使用系統模擬技術，依據分層、模塊化設計思想，制定了空對地攻擊模擬系統總體設計方案；之後根據目前技術狀況，建立了戰斗機機體、推進系統、飛控系統、火控系統、航空炸彈、空地導彈等子系統數學模型；在此基礎上，利用面向對象的軟體設計思想，在基於pc的平臺上開發了一套對地攻擊視景模擬軟體，實現了戰斗機對地攻擊實時視景模擬。
  14. In this dissertation the control loop of attitude angle and collective piston loop are separately. the controller is designed at two scales. and the simulation shows the uncoupling of three attitudes angle loop is achieved with dynamic inversion scheme

    在姿態角通道的設計中，採用了動態逆思想，按照時標分離的原則將直升機飛控系統劃分為快慢迴路，並採用動態逆方法對飛行控制系統進行設計和模擬，模擬結果表明動態逆在通道解耦方面非常有效。
  15. In order to test the anti - disturbance capability of the flight control system, the models of wind shear and turbulence are introduced to the flight control system. the result of simulation shows the flight control system has excellent anti - disturbance capability

    為了驗證飛控系統的抗風擾動特性，引入風切變和紊流，模擬表明所設計的飛控系統對風擾動具有良好的魯棒穩定性。
  16. Fuzzy controller design and stability analysis for flight control systems

    飛控系統模糊控制器設計及穩定性分析
  17. Application of fuzzy mathematics in airplane flight control system ' s fault diagnosis

    模糊數學在飛機飛控系統故障診斷的應用
  18. On integrated design of fault detection and diagnosis modules in flight control systems

    飛控系統多種故障檢診模塊的綜合設計方法研究
  19. Conventional technology of pcs design cannot meet the requirements for quality design

    傳統的飛控系統設計技術很難滿足品質設計的要求。
  20. Design of a robust adaptive reconfigurable flight control system using multiple controllers

    基於魯棒跟蹤控制的飛控系統自適應重構技術研究
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