舵機控制系統 的英文怎麼說

中文拼音 [duòjīkòngzhìxìtǒng]
舵機控制系統 英文
steering gear control system
  • 舵 : 名詞（船、飛機等控制方向的裝置） rudder; helm
  • 機 : machineengine
  • 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...
  • 制 : Ⅰ動詞1 （製造） make; manufacture 2 （擬訂; 規定） draw up; establish 3 （用強力約束; 限定; 管束...
  • 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 ...
  • 控制 : control; dominate; regulate; govern; manage; check; cybernate; manipulate; encraty; rule; rein; c...
  • 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. Segment sliding mode control of missile ' s electromechanical actuation

    導彈電動舵機系統的分段滑模控制
  2. The work module of rudder was discussed and studied by simulation in side jet and aerodynamic compound control manner, the effect on guidance accuracy by control cycle of attitude control engine and action cycle of control loop was simulated

    重點對採用燃氣動力氣動力復合控制方式中舵系統的工作模式進行了探討及模擬研究，對姿控發動機控制周期及控制迴路工作周期對制導精度的影響進行了初步模擬研究。
  3. Considering that electromechanical actuator ( ema ) has the feature of being sensitive to the parameter perturbation and load disturbance, being poor in rigidity etc., deep research has been done to the principle and design method of the ema control system by using the robust control theories

    針對電動舵機存在的易受參數攝動及負載擾動影響、剛度較差的特點，採用魯棒控制理論，對電動舵機控制系統設計理論及方法進行了深入研究。
  4. 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。
  5. It has the characteristic of non - gear - box, large output torque, small volume, easy control, fast response, high track precision, high reliability etc. the system has potential advantages over substituting for traditional hydraulic or pneumatic missile actuator servo control system and has wide prospect in the fields of aerial actuator, servo valve, robot, radar antenna etc. the system ' s operation principle, control idea, functions and realization of each component are discussed in detail

    該系統在取代傳統的液壓、氣動導彈舵機伺服控制系統方面有很大潛力，同時在航空舵機、伺服閥，以及機器人關節的直接驅動、雷達天線等領域具有廣闊的應用前景。論文詳述了系統的工作原理與控制思想，以及系統方案的設計和各組成部分的功能與實現方法。
  6. The study and applications of computer control test system of electrohydraulic control unit for ship rudder

    微機控制船用舵機電液控制單元測試系統的研製及應用
  7. Based on analyzing the operational principles of actuators system, the control strategy and speed regulation of bldcm are described emphatically, and the reason of its torque ripple and the way to eliminating or suppression are analyzed and illustrated, the control algorithms of single dsp to control four actuator of rudder which work independently have been studied, and the design schemes are given

    論文在分析了舵機系統的工作原理基礎上，重點研究了bldcm的調速方法與控制策略，對bldcm的轉矩脈動產生原因及其抑制方法也進行了詳細分析與探討，給出了單dsp控制四個相互獨立工作舵機的控制演算法，並提出了整個舵機位置伺服控制系統的設計方案。
  8. Missile rudders are executive bodies of missile flight control system, all kinds of attitude motion of missile are depended on the actuator driver fins of rudders

    導彈舵機是導彈飛行控制系統的執行機構，導彈的各種姿態運動都是靠舵機帶動舵面偏轉來實現的。
  9. The software designs of the electrical servo system are completed using position loop, speed loop and current loop adjustment after the hardware designs are presented in details. also the efficiency of traditional pid control in practical actuator control system is compared with that of proportional - fuzzy - pid control. at the end of the paper, all factors to affect system performance are analyzed, and optimization designs are presented

    其次論文在詳細介紹舵機控制系統的硬體設計基礎上，完成了系統軟體設計，並採用了位置環、轉速環和電流環的三環控制演算法實現了舵機位置伺服功能，對傳統pid和比例?模糊? pid控制演算法在舵機控制系統中的實際應用效果進行了比較分析。
  10. Finally, the aerodynamic shape optimization design examples for three kinds of reentry vehicles are implemented, which involve a reentry vehicle with cruciform flaps, a variable - bend reentry vehicle and a crew transfer vehicle

    本文的最後，應用智能優化設計系統對帶控制舵機動式再入飛行器、可變彎體再入飛行器以及一種載人返回艙氣動布局這三類工程問題來進行優化設計。
  11. 2. linearizing the fundamental motion equations of the fighters and then establishing the state equations. using nonlinear control system to control the rudder deflexions, and giving decision - making modeling of the maneuver fighting according to the current combat postures of the enemy ' s and our fighters

    2 、通過對空戰飛機基本運動方程的線性化，建立其狀態方程，運用非線性控制系統模型去控制舵面偏轉，並根據敵我機當前的作戰態勢建立機動作戰中的決策模型。
  12. Trapezoid curve method is adopted for frequency control of stepper motor. and a rough speed control method of servo motor is developed. kinematics modeling of rover in manipulation is presented

    控制系統軟體部分採用梯形曲線對步進電機進行升降頻控制，同時實現了對舵機的近似速度控制。
  13. With the help of simulink, fuzzy logic box provided by matlab, s - functions are written in c and m files. the output plots of heading and rudder angle can be obtained. the experiments are performed to test the disturbance rejection properties of the fuzzy model reference adaptive control compared with fuzzy control

    利用matlab提供的simulink動態模擬環境，模糊邏輯工具箱及s -函數，將模型參考模糊自適應控制運用於船舶操舵系統，觀察航向及舵角輸出曲線，然後考慮風、浪及其它隨機干擾，分析系統的抗干擾性。
  14. 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。
  15. Finally according to the performance of unmanned helicopter model, we designed the hardware and software of the servo control system based on a psd3234a mcu. also we built a test platform for the helicopter system

    最後根據無人直升機模型性能，在硬體和軟體上設計並實現了基於psd3234a單片機的舵機控制系統，搭建了一種小型無人直升機模型飛行控制實驗平臺。
  16. This paper studies a data experiment and identification problem of an actual system, in which the steering gear and the satellite - satellite pointing / tracking system act as the study object, based on system identification technique. the main factors that influence identification results and problems that should be paid attention to are analyzed. base on the analysis, auto - regressive moving average with exogenous input model ( armax ) for steering gear and a three - layer predictive control neural network model are established

    從理論的角度研究了對於一個實際系統的數據實驗設計和模型辨識問題，分析了影響系統辨識結果的主要因素以及在辨識過程中應注意的問題，並以此為依據，建立了舵機的滑動平均模型和星星天線指向控制系統的三層預測控制神經網路模型。
  17. Abstract : the control reconfigurable aircraft with multi - surfaces needs robust basic flight control system to support enough time for failure detection and isolation. when partial surface loses, it can keep the damaged aircraft stable. in this paper, multivariable output feedback digital control laws are designed for the control reconfigurable aircraft ( cra ). the method uses fast - sampling digital pi controllers to design digital flight control tracking system. this paper gives the way to design the controller and analyze its robustness characteristics. the simulation results indicate that the controller is very robust and the output responses are fully satisfactory

    文摘:控制可重構飛機要求其基本飛行控制系統對舵面部分缺損故障具有強的魯棒特性，在故障發生后保證飛機的穩定性，提供足夠的時間進行故障的檢測和隔離，為控制系統重構提供條件.本文採用高速采樣pi控制器設計輸出反饋跟隨系統，給出了控制器的設計方法，並分析了它對于控制舵面部分缺損故障的魯棒特性.模擬結果表明，這種控制器具有好的魯棒特性
  18. A new - style missile actuator servo control system is studied in the dissertation

    本文研究了一種新型的導彈舵機伺服控制系統。
  19. The approaches include the modeling, intelligent control and simulation for main diesel marine engine, the designing and development of a single - chip computer based synchronous - meter utilized in ship power station simulation of marine engine room simulator dms - 2000, the software interface of simulation to the ship main engine remote control system aotochief - 4 and the hardware and software development for the ship autopilot control system

    本文對于船舶柴油主機的建模及自動控制，混合智能控制演算法及其模擬；船舶輪機模擬器中的基於單片機的船舶電站模擬並車同步表研製、船舶柴油主機遙控系統「 aotochief - 4 」的模擬軟體界面及船舶自動舵控制軟硬體系統的研製進行了比較詳細的討論。
  20. A pneumatic load - simulator, constructed with a cylinder controlled by proportional valve, is established in this paper, and its characteristics and control strategy are studied

    本文構建了由比例閥控缸實施加載的舵機氣動伺服加載系統實驗裝置，研究其特性及控制策略。
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