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A Methodology for Evaluating Technical Performance Parameter Design Margins to Control Earth and Space Science Instrument Cost.

机译:评估技术性能参数设计裕度以控制地球和空间科学仪器成本的方法。

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摘要

Costs of aerospace missions have increased over the last twenty years, placing the future of the space program in jeopardy. A potential source for such growth can be attributed to the complex multidisciplinary and challenging nature of earth and space science instrument development. Design margins are additional resources carried in technical performance parameters to mitigate uncertainties throughout the product lifecycle. Margins are traditionally derived and allocated based upon historical experience intrinsic to organizations, as opposed to quantitative methods, jeopardizing the development of low-cost space-based instruments. This dissertation utilizes a methodology to evaluate the interrelationships between pre-launch and actual launch margins for the key technical performance parameters of mass, power, and data-rate to identify the extent to which excessive or insufficient margins are used in the design of space-based instruments in an effort to control instrument cost growth.;The research examined 62 space-based instruments from the National Aeronautics and Space Administration, Federally Funded Research and Development Centers, and universities. Statistical analysis consisting of paired t-tests and multiple linear regression were utilized to determine the degree to which space-based instruments are over or under designed by the use of excessive or insufficient design margins and to determine the effect of design margins for the technical performance parameters of mass, power, and data-rate on the percentage instrument cost growth from the preliminary design phase to launch.;Findings confirm, that in the implementation of space-based instruments, design margins are allocated to technical performance parameters above suggested government/industry standards, impacting the development of low-cost space-based instruments. The findings provide senior leadership, systems engineers, project managers, and resource managers with the ability to determine where opportunities exist to make trade-offs to reduce risk and to make informed decisions regarding achieving technical and programmatic requirements. The research forges a paradigm towards statistical analysis as a means to change existing design margin principles in an effort to reduce uncertainties in the design of the space-based instruments, improve the probability of the instruments performing to requirements, and to control cost growth.
机译:在过去的20年中,航空航天飞行任务的成本增加了,这使太空计划的未来处于危险之中。这种增长的潜在来源可以归因于地球和空间科学仪器开发的复杂的多学科性和挑战性。设计裕度是技术性能参数中包含的其他资源,可减轻整个产品生命周期中的不确定性。传统上,利润是根据组织固有的历史经验(而不是定量方法)得出和分配的,这危害了低成本空基工具的发展。本文利用一种方法来评估质量,功率和数据速率等关键技术性能参数的发射前裕度与实际发射裕度之间的相互关系,以确定在空间设计中使用过多或不足裕度的程度。该基础研究旨在控制仪器成本的增长。该研究检查了来自美国国家航空航天局,联邦资助的研发中心和大学的62种天基仪器。利用配对t检验和多元线性回归组成的统计分析,通过使用过多或不足的设计余量来确定天基仪器设计的过度或不足程度,并确定设计余量对技术性能的影响从初步设计阶段到启动阶段的质量,功率和数据速率参数与仪器成本增长百分比的关系;研究结果确认,在实施天基仪器时,设计余量分配给了建议政府/技术指标以上的技术/行业标准,影响了低成本天基仪器的发展。调查结果使高级领导,系统工程师,项目经理和资源经理能够确定在哪里进行取舍以降低风险并就实现技术和计划要求做出明智的决定。这项研究建立了统计分析的范式,以作为改变现有设计裕度原则的一种方法,以减少基于空间的仪器设计中的不确定性,提高仪器达到要求的可能性以及控制成本增长。

著录项

  • 作者

    Jones-Selden, Felicia L.;

  • 作者单位

    The George Washington University.;

  • 授予单位 The George Washington University.;
  • 学科 Engineering Aerospace.;Business Administration Management.
  • 学位 Ph.D.
  • 年度 2015
  • 页码 135 p.
  • 总页数 135
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

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