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Development of a framework for orbital collision avoidance.

机译:开发避免轨道碰撞的框架。

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摘要

Effective systems engineering approaches to actively mitigate orbital collisions of spacecraft and assess the resultant impact are not mature. As the number of spacecraft and density of orbital debris will increase over time, it is logical to expect that all aspects of orbital debris and orbital collisions resulting from debris should be considered for feasible mitigation. The purpose of this dissertation is to develop a framework that employs debris collision avoidance.; A logical and systematic approach to the development of Collision Avoidance Framework (CAF) is proposed, demonstrated, verified and validated. The approach consisted of soliciting collision avoidance-related objectives and priorities from an expert group. The results of the solicitation were documented and incorporated into two different frameworks—one for the case of debris impacting a spacecraft, and the other for the case of a spacecraft impacting another spacecraft.; The CAF was sent to an expanded expert committee consisting of spacecraft operators, as well as US Government and private industry consultants. In addition to evaluating the CAF, the experts provided feedback on additional collision mitigation techniques they employ as well as the feasibility of implementing the CAF.; Actual parameters associated with the collision avoidance decisionmaking process and resultant maneuver that the International Space Station (ISS) undertook on 26 October 1999 are used to validate the CAF. Although the CAF contains financial parameters that were not incorporated into ISS’ decision to avoid collisions, the CAF contains the decisionmaking elements that were embodied in the ISS process.; The experts from both the US Government and private industry asserted that the CAF includes all of the critical elements for making a decision. The utility of CAF lies in its use as a planning aid for investigating “what if” scenarios to ascertain if a maneuver should be executed and to explore the operational and cost implications of such an action. The utility and importance of the CAF can be expected to increase as the number of spacecraft and space debris continues to increase year by year.
机译:主动减轻航天器轨道碰撞并评估由此产生的影响的有效系统工程方法尚不成熟。由于航天器的数量和轨道碎片的密度将随着时间的推移而增加,因此可以合理地考虑,应考虑轨道碎片的各个方面以及由碎片产生的轨道碰撞,以便进行可行的缓解。本文的目的是开发一种避免碎片碰撞的框架。提出,论证,验证和验证了开发防撞框架(CAF)的逻辑和系统方法。该方法包括向专家组征询与避免碰撞有关的目标和优先事项。征集的结果已记录在案,并被合并到两个不同的框架中:一个是碎片撞击航天器的情况,另一个是航天器撞击另一航天器的情况。 CAF被送往由航天器运营商以及美国政府和私人企业顾问组成的扩大的专家委员会。除了评估CAF之外,专家们还提供了有关他们采用的其他减缓碰撞技术以及实施CAF可行性的反馈。国际空间站(ISS)于1999年10月26日进行的与避免碰撞的决策过程和所得演算有关的实际参数用于验证CAF。尽管CAF包含未纳入ISS避免冲突的决策中的财务参数,但CAF包含了ISS流程中体现的决策要素。来自美国政府和私营企业的专家断言,CAF包含了做出决定的所有关键要素。 CAF的用途在于用作计划辅助工具,用于调查“假设情况”场景,以确定是否应执行机动行动,并探讨这种行动的运营和成本影响。随着航天器和空间碎片数量的逐年增加,CAF的效用和重要性有望提高。

著录项

  • 作者

    Keagan, Kathleen Rebecca.;

  • 作者单位

    The George Washington University.;

  • 授予单位 The George Washington University.;
  • 学科 Engineering System Science.; Engineering Aerospace.
  • 学位 D.Sc.
  • 年度 2002
  • 页码 116 p.
  • 总页数 116
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类 系统科学;航空、航天技术的研究与探索;
  • 关键词

  • 入库时间 2022-08-17 11:46:11

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