propulsion control 中文意思是什麼

propulsion control 解釋
推進控制
  • propulsion : n. 推進(力)。 a propulsion engineer 動力裝置工程師。 jet propulsion 噴氣推進。
  • control : n 1 支配,管理,管制,統制,控制;監督。2 抑制(力);壓制,節制,拘束;【農業】防治。3 檢查;核...
  1. Control and propulsion technology of stratosphere airships

    平流層飛艇控制與推進技術
  2. Functioning of and interfaces among propulsion, friction brake, and train - borne master control on rail rapid transit vehicles

    在推動裝置,摩擦閘和鐵路快速運輸車輛的火車上主控裝置之間的介面和功能
  3. Functioning of and interfaces among propulsion, friction brake and train - borne master control on rail rapid transit vehicles

    在推進裝置摩擦閘和軌道快速運輸車輛上的車載主控裝置之間的介面和具備的功能
  4. Distributed real - time simulation system design for integrated flight fire propulsion control system

    戰術任務綜合控制系統分散式實時模擬系統設計
  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. Fourthly, a discussion is devoted to study the integrated flight / propulsion control system

    接著,對新一代殲擊機的綜合飛行/推進控制系統進行研究。
  7. Flight control system and propulsion control system are two of important control systems on an aircraft

    飛行控制系統和推進控制系統是飛機上兩個重要的控制系統。
  8. Simulation is one of the important technologies in the processes of investigation, test, design, and application for aero propulsion control system

    模擬技術是航空推進控制系統研究、試驗、設計和使用中的一項極為重要的技術。
  9. On the basis of designing robust flight control system of the new generation fighter, this dissertation is devoted to the design of the integrated fire / flight control system and the integrated flight / propulsion control system and the integrated fire / flight / propulsion control system

    以研究新一代殲擊機的魯棒飛行控制系統為前提,進一步研究其綜合火力飛行控制系統、綜合飛行推進控制系統以及綜合火力飛行推進控制系統的魯棒控制問題。
  10. Development of simulation technology and its application in aero propulsion control system are introduced firstly, then the engineering design are carried out based on the concept design for monitoring system of the simulation test platform. starting with analysis of function requirement of the monitoring system, signal interface, resource configuring and monitoring software are designed

    論文首先介紹了模擬技術的發展以及在航空推進控制系統中的應用,接著對半物理模擬平臺的監控系統在概念設計的基礎上進行了工程化設計,從監控系統功能需求分析入手,設計了監控系統的信號介面、資源配置以及監控軟體。
  11. With above principles, take domestic and abroad research works as foundation, this paper try to improve the degree of integration and automatization of aircraft based on currently available technology and equipment. the study focus on how to realize auto - flight and auto - attack through the integration of flight control, fire control and propulsion control system, a satisfied result wold be feasible system integration schemas that could improve the mission performance and enhance the aircraft combat automation

    基於以上考慮,本文參考國內外已經完成的工作,致力於在現有技術基礎上提高飛機綜合化、自動化程度,研究通過飛行、推進、火控等系統的綜合實現自動飛行、自動攻擊的原理、演算法,提供可以工程應用的系統綜合方案。
  12. With respect to the issue of integrated flight / propulsion control system design, adopting the decentralized solutions of system integration, this article studied the key technologies in this integrated control system, based on which a real - time integrated closed - loop model of plane / engine was built and a study of variable structure control of integrated flight / pro - pulsion control system was conducted. through a great many simulations, the feasibility of the solution was verified and a simulating platform of integrated flight / propulsion control system was designed and developed by utilizing directx multi - media development libraries

    本文針對飛行/推進綜合控制系統設計問題,採用分散的系統綜合方案,研究了飛行/推進綜合控制中的關鍵技術,在此基礎上建立了飛機/發動機綜合閉環實時模型,進行了發動機的變結構控制研究,通過大量的模擬,驗證了控制方案的可行性,並基於directx多媒體開發庫設計完成飛/推綜合控制系統模擬平臺界面的開發。
  13. This primary module can also be applied in the research of advanced control applications, such as integrated flight - propulsion control, distributed aero engine control, and so on

    該模塊也可作為飛推綜合控制、分散式控制等需要高性能計算能力和實時數據通信的核心電路模塊使用。
  14. Epcs electronic propulsion control system

    電子驅動力控制系統
  15. Study on an integrated fire flight propulsion control system and its digital simulation design platform

    推綜合控制系統及其模擬平臺研究
  16. Integrated flight / propulsion control ( ifpc ) is the trend of aircraft and aero - engine control

    飛行推進系統綜合控制是未來先進飛機和發動機控制的發展趨勢。
  17. Now people pay more attention to the issue of integrated flight / propulsion control, which is an unnegligible newcome trend

    人們開始把注意力集中到飛行/推進綜合控制課題上來。這個不可忽視的新趨勢正在進展之中。
  18. A design method of integrated flight / propulsion control ( ifpc ) optimization computer based on digital signal processor ( dsp ) and control area network ( can ) bus is presented

    本文提出基於dsp和can總線的飛推綜合控制優化計算機設計方案,並研製成功原理樣機。
  19. In order to meet these requirements, the aeronautical propulsion system has to provide more powerful and sustainable force. this also poses new requirements for propulsion control system. as a result, integrated propulsion system performance seeking control is introduced

    要達到這一目標,航空推進系統必須能夠提供更強大更持久的動力,這也對推進系統的控制提出了新的更高的要求,為此需要對推進系統進行最優控制規律研究。
  20. In this book the methodology and concept of designing multivariable control systems for aeroengines are presented which include : general development tendencies in aeroengines and aeroengine control systems ; modeling of aeroengines ; design of various control laws for aeroengines ; design of fault tolelant control systems for aeroengines and design of integrated flight / propulsion control systems

    本書闡述現代航空發動機多變量控制系統設計方法及概念:航空發動機及其控制系統的發展趨勢;航空發動機建模;各種航空發動機現代控制規律的設計;發動機容錯控制系統設計以及飛行/推進綜合控制系統設計。
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