mission simulation 中文意思是什麼

mission simulation 解釋
任務模擬
  • mission : n 1 派遣；國家代表團的派遣；代表團；使團；（伊斯蘭教的）朝覲團；特使；〈美國〉駐外使節，大[公]使...
  • simulation : n. 假裝；模擬；裝病，裝瘋；【生物學】擬態，擬色。
  1. Then this paper briefly introduces the mission planning system of cruise missile, analyzes the characteristic of intelligent decision modeling in virtual battlefield. considering the simulation of warplane, this paper puts forward agent - based method of intelligent decision modeling which meets the demand of military simulation. therefore a multi - agent system ( mas ) can be established to deal with collaboration and cooperation in team

    分析了虛擬戰場中智能決策建模的特點，結合作戰飛機的模擬介紹了決策建模的過程和方法，提出了適合於軍事模擬需求的基於智能體的決策建模方法，以此為基礎可構成多智能體系統以有效地處理成員之間的協作。
  2. The simulation of " flight mission 3d visualization of the unmanned aerial vehicle ( uav ) " fully absorbs and applies current advanced 3d visualization theory, simulates the characteristics of true 3d volumetric display technique which are full - vision, multi - angle and can be observed by many persons at the same time and so on. it displays the process of flight according to mission of uav by the online of four computers

    「無人機任務飛行的三維可視化」模擬充分吸收和運用當前先進的三維可視化理論，盡可能的模擬真三維立體顯示技術的全視景、多角度、可供多人同時觀察等的特點，通過四臺計算機的聯機，在同一時刻從各個不同的角度來顯示無人機任務飛行的全過程。
  3. Chapter 4 studies scheduling algorithm of the core node to implement on single adsp2191. the result shows that a single adsp2191 chip can ’ t satisfy the bhp processing delay request and parallel processing is inevitable. chapter 5 primarily studies the core node ’ s scheduling algorithm with many dsp parallel process. details of lauc - vf scheduling algorithm analysis data flow organization and mission distribution are argued. the results of software simulation and hardware debugging indicate that many dsp parallel processing is effective and coincident with the system ’ s demand

    結果表明單片adsp2191晶元不能夠滿足核心節點對bhp的實時處理要求，必須多dsp并行處理。第五章研究了核心節點調度演算法的多dsp并行處理。對多bhp批調度演算法的實現進行分析，探討了多bhp處理任務的的劃分和分配方案;多dsp間數據通信和傳輸的dma實現;最後對多處理器并行的處理時間進行模擬測試分析。
  4. Due to mission profile, launched conditions and trajectory, maneuver chains for stand off missile are designed. instruction control model and maneuver model is setup for ucav flight simulation

    結合作戰任務剖面、導彈發射條件和彈道，設計出無人機防區外攻擊導彈發射前、后的機動動作鏈。
  5. After discuss the structure and character of operating system qnx and inter - process communication between pc ' s running qnx or windows, the paper describes the structure, function and flow chart of mission planning software which is developed in qnx, and narrates the course of simulation co - debug experiment, dynamically showing the results of the mission planning in the case of " ocean physiognomy reconnaissance ", and proving the logical correctness and feasibility of task serial produced by mission planning

    在論述了多任務、實時操作系統qnx的結構特點以及基於qnx與windows運行的pc機之間網路進程通信的基礎上，本文描述了在qnx上開發的使命規劃軟體的結構功能和流程圖，並敘述了模擬聯調實驗的過程，動態地顯示了「海洋地貌勘測」這一案例使命規劃的結果，並證明了使命規劃所得的任務序列在實際運行中邏輯的正確性與可行性。
  6. The main mission of simulation is to help trouble removal people reconnaissance field, calculate parameter and analyze causality fast. and with these, the reason for accident, the policy on how to avoid accident and minimize loss will be conclude

    其主要任務是輔助事故處理人員快速、高質量地進行現場勘察、參數計算和因果分析，進而研究事故發生的原因，探求避免事故、減少損失的策略。
  7. Due to mission requirements, the pd depth control arithmetic is designed and the simulation result is provided. in order to reduce heading control bias, the compass data bias is corrected

    為提高航向控制精度，對航向控制系統中的磁通門傳感器的誤差進行分析，並提出了誤差校正的方法。
  8. The paper mainly does research on simulation of the air - to - surface ( as ) attack mission. on the basis of that, as attack representative maneuver chains are designed. and, corporation between uninhabited combat air vehicle ( ucav ) and as missile is discussed in the process

    本文主要針對無人機對地攻擊任務特點，開展模擬模型研究，並以此為基礎設計出無人機防區外攻擊的典型動作鏈，對攻擊過程中無人機與空地導彈的配合問題進行了初步的研究。
  9. Analysis on the stk - based space mission simulation

    的航天任務模擬方案分析
  10. The data collection mission is important in distributed simulation systems. the data collection and fom agility problems are solved in the framework. based on the dynamic object model representation, an adaptive data logging policy is proposed in yh - fwf, which can meet the new requirements of hla distributed simulation system data collection mission

    數據採集是分佈模擬系統中的重要任務， hla分佈模擬系統的數據採集任務具有一些新的特點，本文提出以對象模型動態表示為基礎，在yh - fwf框架中以可接入的方式提供數據記錄能力，很好地解決了hla模擬過程中的動態數據採集問題。
  11. Based on mission planning technique and distributed interactive simulation ( dis ), a virtual drone simulation system that has novel applications is developed

    在此基礎上，基於任務規劃技術和分散式交互模擬技術，開發了一個基於dis的防空訓練空情保障系統。
  12. Simulation based mission reliability calculation methods of complex weapon system

    應用橋接成員實現高層體系結構多聯邦互連
  13. In this thesis, firstly, we make a concise comparison and analysis of the popular fdtd software, introduce the electromagnetic simulation software ( gems ) developed by our group, and present the shortage of this software to show the mission of this thesis. chapter 2 presents the principle of the algorithm, including its four key techniques : curved metallic surfaces, curved dielectric surfaces, non - uniform mesh, and treatment for lossy dielectric

    論文第一章首先概述了國內外目前基於時域有限差分法相關軟體的發展狀況，對各軟體的內外部結構及特點做了比較和分析，然後對本課題組開發的模擬軟體（ gems ）的前期版本進行了簡單介紹，並指出其不足之處，說明該課題工作的意義和特點。
  14. Functional description of mission space ( fdms ) is the first abstract of real world and the functional description that is independent of simulation realization and the common start point of authoritative and coherent m & s. to provide the authoritative, correct and normative knowledge description of real world is one of the goals for fdms

    使命空間功能描述（ functionaldescriptionofmissionspace ， fdms ）是對真實世界的第一次抽象，是獨立於模擬實現的、與某項軍事使命相關的實體、活動、任務、交互和環境等因素的功能描述，是建立權威和一致的m & s的公共起點。
  15. In 2000, the study on insar surged up worldwide due to the successful shuttle radar topography mission ( srtm ) developed by nasa etc. now, efficient and accurate data processing and simulation of insar are still the main problems in this area

    2000年美國srtm全球地貌測繪計劃成功運行，掀起了世界范圍內干涉sar研究的高潮。目前，高效、精確的干涉合成孔徑雷達數據處理和模擬研究仍然是該領域所面臨的主要問題。
  16. Typical results are given to calculate mission success probability etc. in air - to - ground radar electronic combat by modeling and simulation. computer simulation is higher fidelity and full - scale than static analytical analysis, also is more flexible and lower cost than field test

    說明這種方法比經典的靜態解析分析評估法要全面和逼真，比外場實物試驗要廉價和靈活，並且面向對象的模擬模型庫可以方便地擴展到其它場景下的雷達電子戰作戰效能評估。
  17. Simulation results indicate that the closed - form guidance law with robustness is fit to the finite propulsive reentry mission and insensitive to the initial position errors, propulsion direction errors and observation errors

    模擬結果表明，該閉路初制導能夠完成有限推力情況下的再入初制導任務，對初始位置誤差、推力方向偏差和測量誤差不敏感，具有一定的魯棒性和適應性。
  18. From the hiberarchy of sos, the concept of sos structure evolution simulation of the armament sos was introduced, and the mission and holistic idea of sos structure evolution simulation were analyzed

    從武器裝備的體系層次出發，提出了武器裝備體系結構演化模擬的概念，明確了體系結構演化模擬的使命任務及總體思路。
  19. In the end, to realize modeling using the template in this paper, simulation system of modeling and mission planning for deep space explorer is designed and realized with java language

    為實現探測器自主規劃系統建模的快捷化和智能化，本文提出了模板化的黑箱建模方式。最後，採用java語言，設計並實現了深空探測任務建模/規劃系統平臺。
  20. In this thesis, based on the available research of this field, the method to resolve the constraint conditions of the optimization problems has been improved and the parametric sensitivity analysis of the trajectory optimization has been completed. guided by object - oriented method and considering the mission needs and user requirements adequately, the hierarchical structure of the system is analyzed. the uml ( unified modeling language ) is also applied to establish the simulation systems framework

    本文在已有研究的基礎上，對優化問題的約束處理方法進行了改進，並完成了軌跡優化問題的靈敏度分析，在面向對象方法學的指導下，根據系統的優化模型和優化策略，分析了系統的層次結構，並基於uml建立了模擬系統框架，運用泛型技術進行程序設計，最終實現了運載火箭性能優化軟體。
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