flight engineering 中文意思是什麼

flight engineering 解釋
隨機工程師的職責
  • flight : n 1 飛行，飛翔；（鷹對獵物的）追趕。2 （候鳥等的）遷徙；飛行的一群。3 （光陰）飛逝。4 （思想等的...
  • engineering : n. 1. 工程（技術），工程學。2. 開車技術。3. 土木工程，工事。4. 操縱，管理。
  1. Uav ( unmanned aerial vehicle ) plays a more and more important role in national defense and civil life. so making researches on the uav flight controller design and the measurement and control techniques of uav is of theory, engineering and economical value

    無人機在軍民兩用領域發揮著越來越重要的作用，進行民用無人機飛行控制器設計及檢測與控制技術研究，具有理論意義、工程意義和經濟意義。
  2. Aviation engineers are designing a more environmentally sustainable airplane that may overturn long - held notions of flight engineering

    航空工程師們目前正探討設計新一代的綠色環保飛機，那將在很大程度上顛覆傳統的飛行工程學設計理念。
  3. During the development of real - time application software systems for space - flight engineering, various model tests of missiles weapons, and dynamic model tests of cruise missiles, software testing has been a significant problem of quality control that remains to be solved

    在航天工程、導彈武器多種型號試驗任務的各項計算機實時應用軟體系統的研製過程中，軟體測試問題是保證各大系統軟體質量所面臨的亟待解決的問題。
  4. In addition, some problems about engineering applications including the influence of regulating parameter to system control effect and the adaptability of the model following controller in flight envelope are discussed

    此外，文中對控制器中的可調參數對控制效果的影響及最終滑動模態變結構模型跟蹤控制器在飛行包線范圍內的適應性等工程應用問題進行了討論。
  5. 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。
  6. Applications to aerospace engineering are discussed, including introductory topics in orbital mechanics, flight dynamics, inertial navigation and attitude dynamics

    亦將討論動力學在航太工程上的應用，包含軌道力學，飛行力學，慣性導航與姿態動力學。
  7. As one of main branches of the automatic control and signal processing, system identification has played a more and more important role in many fields, such as space - flight, aviation, engineering control, chemistry, finance and so on

    系統辨識技術是自動控制、信號處理等學科的主要分支之一，在航天、航空、工程式控制制、化學、金融等領域日益發揮出重要作用。
  8. 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。
  9. Target state estimater ( tse ) is an important and indispensable part of integrated flight and fire control system ( iffcs ). this article takes the ground mobile object as the study model. it established the system state equation and observation equation from the perspective of promoting system accuracy, simplifying the calculation and facilitating the engineering realization, the tse was set up by using the kalman filtering calculation method in the wake of linearizing the observation equation to make it adapt the precondition

    目標狀態估計器是綜合飛行/火力控制系統中的一個重要組成環節，本文以地面機動目標為模型，從提高目標估計精度、簡化計算以及便於工程實現為出發點，建立目標的狀態方程及觀測方程，並對其進行線性化，利用自適應卡爾曼濾波演算法構造目標狀態估計器。
  10. The training programmes delivered in the hong kong civil aviation training center cover areas on air traffic management, airport standards, engineering and systems, flight standards and airworthiness, and air services

    民航訓練中心提供的訓練課程相當廣泛，涵蓋航空交通管理、機場標準、工程及系統、飛行標準和適航以及航班事務等各個范疇。
  11. Jdpdm is a pdm system sustaining flight vehicle concurrent design which is developed by china aviation industry corporation. this thesis adopts the fashionable object - oriented method and unified modeling language ( uml ) to analyse, design and realize systems. first, this thesis introduces development and application of concurrent engineering and product data management both home and abroad. second, we make system analysis of jdpdm and analysis the functions of document management and vault. third, we supplement the specification, and we design and realize models of document management and vault based on pdm enablers. last, this thesis presents whole - length work summarization and suggestions of more research

    論文首先介紹了國內外并行工程與產品數據管理技術的發展與應用;其次，對jdpdm進行了詳細的系統分析及文檔管理和電子倉庫模塊的功能分析;再次，在深入研究pdmenablers規范的基礎上，依據項目實際需求，對原規范進行了一定的擴充，在此基礎上提出了基於pdmenablers的文檔管理與電子倉庫模型並對其進行詳細設計及實現;論文的最後給出了全文的工作總結與進一步研究的建議。
  12. Experimental modal analysis based on ambient vibration is mainly to deal with the engineering problems from with we can hardly achieve the input signals, such as the operational modes of a flight vehicle during the flight or the dynamic behavior of a large - scale structure like an offshore platform, a bridge as well as a skyscraper on which we can ’ t exert a heavy kick

    基於環境振動的實驗模態分析主要針對一些激勵不可測的工程問題，如研究飛行器在飛行中的運行模態，或諸如海洋平臺、橋梁、摩天大樓之類難以施加激勵的大型結構的動態特性。本文重點研究了隨機子空間方法在環境振動模態分析領域的應用。
  13. Full - service maintenance and completion facility for helicopters. provides airframe service for all major manufacturers, engine service, completion services, engineering ( das and der ' s ), and flight sales and management

    為直升機提供整套維修，包括機身服務、發動機服務、工程設計、飛機銷售和管理等。
  14. Nonlinear dynamic inversion control law can better solved the control problem of super - maneuver flight. consider the engineering implement and the idiographic request of air force equipment department, this thesis used c + + programming language to describe dynamic inversion control law and model of the fourth generation fighter. for the convenience of user interface and maintenance, we encapsulated the software as a dll

    考慮到工程實現和空軍裝備部的具體要求，本文採用c + +語言來對動態逆控制律以及第四代殲擊機模型進行描述，為了用戶介面和維護的方便，在此基礎上使用dll動態鏈接庫的形式對軟體進行了封裝。
  15. 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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