simulation control subsystem 中文意思是什麼

simulation control subsystem 解釋
模擬控制子系統
  • simulation : n. 假裝;模擬;裝病,裝瘋;【生物學】擬態,擬色。
  • 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...
  • subsystem : n. (系統的)分部;分體系,支系統。
  1. Engine load simulated control system was consisted of two unattached parts of work resistance simulated control subsystem and electric bow wave dynamometer control subsystem. with the mathematic models of engine load simulation controller, which transferred the work resistance ' s change to engine load change immediately, the system can met the need of the simulation control system

    發動機負荷模擬加載控制系統包括彼此獨立的作業阻力模擬控制子系統和電渦流測功機控制子系統兩部分,應用發動機負荷模擬控制器數學模型,使作業阻力的變化及時轉換為發動機負荷的變化,能夠滿足模擬系統的控制要求。
  2. In this dissertation, the data process ( dp ) subsystem and radar control program ( rcp ) subsystem of gbr simulation system have been studied and discussed. the main work and innovation of this dissertation is as follows : ( 1 ) track filter, the basic element of track system, has been researched. we analyze the advantage and disadvantage of common target kinematic model such as constant velocity model, constant acceleration model, noval statistic model

    本文是基於某gbr模擬系統的合作項目中,本人負責的數據處理子系統和雷達控製程序子系統的研究和開發的結果,主要進行的工作和創新有: ( 1 )基於跟蹤系統最基本的要素-跟蹤濾波,分析了當前常用的微分多項式模型, cv與ca (常速與常加速)模型,時間相關模型, noval統計模型,以及機動目標「當前」統計模型等目標運動模型的優缺點和雷達的觀測誤差。
  3. The thesis describes the conception of the object - oriented modeling and integrated simulaton enviroment, and discusses the below topics : ( 1 ) describe the reasonable structure of the modern fighter simulation system, and design the data transfer interface. ( 2 ) discuss the modeling method of the key subsystem of future fighter system especially the aerodynamics and the control system in detail. ( 3 ) construct the 3d model of the aircraft and scene, and verify the graphic simulation technique based on pc

    本文詳細討論了面向對象建模方法以及一體化模擬環境的基本概念框架及基本結構並在此基礎上提出了合理的現代戰斗機模擬系統結構,設計了模擬系統的數據傳遞介面;詳細討論了現代戰斗機模擬系統關鍵子系統? ?飛機本體、飛行控制系統建模方法;建立了用於研究的飛機以及視景的三維顯示平臺;並在此基礎上實現了實驗性的基於pc的現代戰斗機圖形模擬平臺,對模擬模型有效性確認和驗證工作做了初步的探討,研究比較了傳統飛行動力學和運動學方程和四元數法在飛行模擬中的效果。
  4. In the control scheme using neural network, the control of flexible manipulator is separated into angle - following control of slow subsystem and vibration - suppressing control of fast subsystem based on singular perturbation and time decomposition. moreover, the paper discusses the structure and the algorithm of neural network plus fuzzy pd control of tip vibration. finally the performance of designed methods is validated by simulation

    對于神經網路控制,首先根據奇異攝動和兩時標分解,將柔性連桿機械臂的控制分解成等效剛性臂慢子系統的角跟隨運動控制和快子系統的消振控制,論文給出了神經網路+末端振動模糊pd控制的結構和計演算法,並通過實驗研究驗證了提出設計方法的性能。
  5. Weaponry photoelectric simulation system is composed of the infrared object and scene generated subsystem, exploring and tracking simulation subsystem, movement simulation platform, simulation analysis evaluation subsystem and simulation control with visual display subsystem

    兵器光電模擬系統由紅外目標場景產生子系統,探測跟蹤模擬子系統,運動模擬平臺,模擬分析評估子系統,模擬控制與形象化顯示子系統構成。
  6. The small astronomical satellite has demands on both pointing accuracy and attitude maneuverability, so this thesis modeled the attitude control subsystem based on reaction wheels. under the fine precision pointing mode, a pd control law and a variable structure ( vs ) control law were studied respectively, and the simulation validated that vs control is more effective under fine precision pointing mode. furthermore, the vs controller for rapid large - angle maneuver was also designed

    2 ) svom衛星同時對指向精度和姿態機動性有著很高的要求,因此本文建立了基於反作用飛輪的svom衛星姿態控制系統模型,在高精度慣性定向三軸穩定模式下分別設計了pd控制律和變結構控制律,通過模擬驗證了變結構控制對于svom衛星的有效性,並基於變結構控制研究了svom衛星快速大角度機動的方法。
  7. The overall modal of test - bed for test & control system is built, based on deeply analysis of thermal torpedo ' s power & propelling system in a overall design view. in the paper, the general building of test & control system, the building of all parts " simulation model ( subsystem or module ), testing software designing and rotation rate control designing are discussed mainly

    本文在對魚雷熱動力推進系統性能深入研究的基礎上,完成了動力推進系統測控系統試驗臺的研製,包括測控系統總體設計、各模塊模擬模型建立、測試軟體設計及轉速控制器研製等主要內容。
  8. For the convenience of study, a simulation control system of tractor - implement combination was designed, which had the characteristics of reasonable structure, simple and practical. the control system was composed of three parts : master pc monitor system, transmission and throttle control subsystem, engine load simulated control subsystem. using the system could take many studies on implement units

    為研究方便,本文首先設計了結構合理,簡單實用的拖拉機作業機組模擬試驗控制系統,控制系統由上位機監控系統、發動機及換擋控制系統、發動機負荷模擬加載控制系統等三大部分組成,利用本控制系統能對機組進行各種加載試驗研究。
  9. A computer control simulation for the compressed air subsystem was performed. from the simulation we can see that the computer perform the logic control exactly. the system runs safely and smoothly

    通過模擬實驗可以看到,系統能按照實際工作流程運行工作,計算機能準確的執行所編制的邏輯控制,使系統安全、正常的運行。
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