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Accurate vision measurement for kinematic parameters of satellite separation tests
  • ISSN号:1001-506X
  • 期刊名称:《系统工程与电子技术》
  • 时间:0
  • 分类:TP391.9[自动化与计算机技术—计算机应用技术;自动化与计算机技术—计算机科学与技术] TU20[建筑科学—建筑设计及理论]
  • 作者机构:[1]College of Aerospace and Materials Engineering, National University of Defense Technology, Changsha 410073, China, [2]Faculty of Aerospace Engineering, Delft University of Technology, 2629HS Delft, the Netherlands
  • 相关基金:Foundation items: National Natural Science Foundation of China (50975280, 61004094); Program for New Century Excellent Talents in University (NCET-08-0149); Fund of Innovation by Graduate School of National University of Defense Technology (B090102); Hunan Provincial Innovation Foundation for Postgraduate, China.
中文摘要:

包括地估计 fractionated 太空船,一个评价工具在模块化的进化随机的模型驾驶的无常下面基于生命周期模拟被开发。首先, fractionated 太空船名称和建筑学被澄清,并且评价标准被分析。风险的平均数和标准差调整了生命周期费用和在场的网价值(NPV ) 被定义为评价度量标准。第二, fractionated 太空船缩放模型简短被描述,由风险的详细讨论列在后面调整生命周期费用和 NPV 模型。第三,在 fractionated 太空船生命周期上的无常来源与概率被分析并且当模特儿理论。然后,按年代先后的生命周期模拟过程被详细说明,并且模拟模块与面向对象的方法论被开发建立评价工具。前面的无常模型集成于这些模拟模块,因此随机的目标地位能与生命周期时间安排被模仿并且演变。调查 fractionated 太空船因为一个假想地球观察使命与建议评价工具被执行的案例研究,和结果证明那分别度和发射表明在费用和 NPV 上有大影响,并且通常 fractionated 太空船是比它在无常效果下面的整体的对应物更先进的。最后,一些结论被给,未来研究话题被加亮。

英文摘要:

To comprehensively assess fi'actionated spacecraft, an assessment tool is developed based on lifecycle simulation under uncertainty driven by modular evolutionary stochastic models. First, fractionated spacecraft nomenclature and architecture are clarified, and assessment criteria are analyzed. The mean and standard deviation of risk adjusted lifecycle cost and net present value (NPV) are defined as assessment metrics. Second, fractionated spacecraft sizing models are briefly described, followed by detailed discussion on risk adjusted lifecycle cost and NPV models. Third, uncertainty sources over fractionated spacecraft life- cycle are analyzed and modeled with probability theory. Then the chronological lifecycle simulation process is expounded, and simulation modules are developed with object oriented methodology to build up the assessment tool. The preceding uncertainty models are integrated in these simulation modules, hence the random object status can be simulated and evolve with lifecycle timeline. A case study to investigate the fractionated spacecraft for a hypothetical earth observation mission is carried out with the proposed assessment tool, and the results show that fractionation degree and launch manifest have great influence on cost and NPV, and generally fractionated spacecraft is more advanced than its monolithic counterpart under uncertainty effect. Finally, some conclusions are given and future research topics are highlighted.

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期刊信息
  • 《系统工程与电子技术》
  • 北大核心期刊(2011版)
  • 主管单位:中国航天科工集团公司
  • 主办单位:中国航天科工防御技术研究院 中国宇航学会 中国系统工程学会
  • 主编:施荣
  • 地址:北京142信箱32分箱
  • 邮编:100854
  • 邮箱:xtgcydzjs@126.com
  • 电话:010-68388406
  • 国际标准刊号:ISSN:1001-506X
  • 国内统一刊号:ISSN:11-2422/TN
  • 邮发代号:82-269
  • 获奖情况:
  • 全国中文核心期刊,全国优秀科技期刊,中国科技论文统计用刊,中国期刊方阵“双百”期刊
  • 国内外数据库收录:
  • 德国数学文摘,荷兰文摘与引文数据库,美国工程索引,美国剑桥科学文摘,英国科学文摘数据库,日本日本科学技术振兴机构数据库,中国中国科技核心期刊,中国北大核心期刊(2004版),中国北大核心期刊(2008版),中国北大核心期刊(2011版),中国北大核心期刊(2014版),中国北大核心期刊(2000版)
  • 被引量:34341