airplane control 中文意思是什麼

airplane control 解釋
飛機的操縱
  • airplane : n. 〈美國〉 飛機〈英國說 aeroplane〉。2. vi. 坐飛機。
  • 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. Thus, we can construct high performance airplane optic fiber control system on the basis of it. the existing avionic system has already set higher standard of the exchanging capability the data information

    As1773總線具有可靠性高、抗電磁干擾能力強、重量輕、組網方式靈活等優點,可在它基礎上組成高性能的飛機光傳操縱系統。
  2. The thesis roots in the item supported by " fifteen " aviation funds, - new type aeronautic linear dc motor ( ldcm ), study its classes characteristics and work principle, mainly researches the drive and control technique of aeronautic linear dc step motor ( ldcsm ) using in emergency discharging oil valve on airplane

    本文源於「十五」航空支撐基金項目-新型航空用直線直流電動機。論文研究了直線直流電動機的分類、特點及其工作原理,重點針對飛機應急放油閥用航空直線直流步進電動機驅動控制技術進行了研究。
  3. Development of electromechanical actuation system for flight control is one of the most important technologies in the path to all - electric airplane

    摘要飛行控制中機電作動系統的發展是全電飛機的重要技術之一,而高速大功率密度的無刷直流電動機是其中的關鍵部件。
  4. Focusing on the flight control computer system of some type of airplane, this paper first analyzes the advantage and disadvantage of the structures of many kinds of fault tolerant flight control computer systems and their ability in tolerating fault, followed by summarizing the key design technology. the dual similar redundancy fault tolerant computer system is brought forward as the design scheme for the required flight control computer. also brought forward is the particular system design

    本文以某型號飛機飛控計算機系統為研究對象,首先分析了各種類型容錯飛控計算機體系結構的優缺點及容錯能力,總結了容錯計算機系統設計的關鍵技術,然後提出了二模相似余度容錯飛控計算機系統設計方案,詳細設計了以motorola公司生產的先進powerpc740微處理器為核心處理器、以高性能的國際標準化通用vme總線為內總線的交叉通道通信容錯計算機系統。
  5. It has solved the problem of weak robust when the linear control theory is used to control a complicated nonlinear systems like airplane

    克服了單純用線性控制系統理論來控制象殲擊機這樣的復雜非線性系統魯棒性能較差的問題。
  6. These advantage make it excellent materials for control surface, wing and skin of airplane

    是飛機結構中對剛度要求較高的操縱面、機翼和機身蒙皮結構用較理想的材料。
  7. This perfect control made their sliding safe and allowed them to proceed to the powered airplane.

    這種完善的操縱機構,使他們能安全滑翔並進一步製造有動力裝置的飛機。
  8. This paper presents a simulation test control system of an airplane engine operating system, which control motor to simulate the force and velocity of throttle lever and the torque on axis

    本文闡述了某型飛機發動機操縱系統地面模擬試驗控制系統,它主要控制力矩電機去模擬油門桿上的速度和力以及模擬發動機輸入軸的力矩。
  9. After a misunderstanding aboard an airplane that escalates out of control, the mild - mannered dave buznik is ordered by judge daniels to attend anger m.

    經過一次罕有地在飛機上跟人口角之後,被送到處理憤怒治療師畢地的珍所接受觀察,畢地教他要好好利用憤怒平衡心理
  10. His son was trying to control the airplane and he just couldn t control it and pretty soon it started doing circles. every circle got bigger and bigger and bigger and all of a sudden ka - boom

    飛到空中了,兒子試著去控制它,但卻控制不了很快,那飛機在半空中,開始打轉,每一圈都比先前的更大更大更大
  11. 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
  12. Study on cost control of modern airplane manufacturing

    現代飛機製造成本控制方法研究
  13. Research on airplane noise and the strategy of control

    飛機噪聲及防治對策的研究
  14. To seize control of an airplane, boat, automobile, etc

    強行控制飛機、船隻、車輛等。
  15. This paper is developed a algorithm to generate airplane ' s 4d approach trajectory, by using fourth order runge - kutta, based on a set of point mass equations of motion, pilot procedure and air traffic control procedure

    本論文是基於飛機質心運動方程組,結合飛行操作程序和空管管製程序,根據飛機的空氣動力學模型、推力模型和實時的大氣氣象模型,用四階龍格? ?庫塔積分法規劃出飛機下降進近4d軌跡。
  16. According to the information management system developed for the standard part workshop, chengdu airplane company ( cac ) to realize its agile and cooperative work, this paper puts forward an architecture of virtual workshop management and control, implementing model of virtual workshop production scheduling and management system based on multi - agent principle, programming technology and method of constructing knowledge management system

    本文以實現成都飛機公司標準件製造車間的敏捷性和協同作業需要為實際背景,研究了虛擬車間管理與控制的體系結構、基於多智能體技術的虛擬車間生產作業規劃與管理系統的實施方法、網路編程技術及虛擬車間中調度和知識管理問題。
  17. The project originating from national high technology research development plan ( 863 plan ) is to study a control system of 270 voltages dual - redundancy rare earth permanent magnet ( repm ) brushless dc motor ( bldcm ) based on digital signals processor ( dsp ) in order to realize precise and reliable control for the control actuator of high altitude unmanned airplane

    本課題來源於國家高技術研究發展計劃( 863計劃) ,旨在研究基於數字信號處理器( dsp控制器)的舵機用270v高壓雙余度稀土永磁無刷直流電動機控制系統,以實現無人飛行平臺飛控系統的精確可靠控制。
  18. A new method is developed to predict the temperature distribution of cooling - plate with non - uniform heat load on the surfaces, meanwhile, two types of cooling - plate used in the environment control system of airplane are studied experimentally under conditions of different reynolds number of air and surface heat loads

    摘要提出了一種新的冷板簡化數學模型,把翅片摺合成導熱系數?各向異性的等效厚度層實芯板,將冷板與空氣的對流換熱作?等效層的穩態導熱問題,計算了表面熱源非均勻條件下冷板的溫度分佈。
  19. 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。
  20. During the procedure, the airspeed continues accelerating ( or decreasing ) and the aircraft configuration is rapidly changing. the aerodynamic interactions are complex and lead to dynamic instabilities. the shift between helicopter and airplane flight modes necessitates a change in control strategy

    過渡模式下,飛機速度不斷增加(或減小) ,氣動布局不斷改變,飛機動力穩定性差且氣動干擾嚴重,直升機控制和固定翼控制切換,因此過渡模式動力學特性和控制系統研究是整個傾轉旋翼飛機研製的主要難點。
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