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A Reliability Estimation Tool for Reducing Infant Mortality in CubeSat Missions

机译:一种可靠性估计工具,用于减少幼态特派团婴儿死亡率

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For many years, traditional satellite design philosophy was dominated by highly reliable components, conservative designs and extensive performance testing at subsystem and integrated system levels to achieve long lifetimes in the harsh space environment. CubeSats attempted to choose a different philosophy, utilizing suitable state-of the art, commercial-off-the shelf products, yielding, if successful, an increased performance per mass figure of merit for those small vessels at potentially higher risk but lower cost. CubeSats seemed to promise universities and companies to be faster, better and cheaper-once more in history. Unfortunately, many CubeSat missions, especially university-built ones, never achieved a detectable functional state or failed shortly after the satellites were ejected from their deployer. Data based on our developed CubeSat Failure Database (CFD) and research carried out by others suggest, that a great percentage of those early failure cases could have been detected and avoided by more careful and adequate system-level functional testing on the ground. However, many university teams still fail to plan with adequate resources for system level functional testing or are confronted with hard deadlines, thus unable to complete appropriate integrated system testing on a sufficient level, and launching a satellite that never was adequately functional. Ongoing work on a novel reliability estimation tool using Bayesian methods is introduced to fill this gap and to provide meaningful data for all developers on the achievable reliability and required functional testing time of their CubeSats. Using test data and reliability goals for their actual mission, merging that data with statistical data from past missions and a database of subjective developer's beliefs, CubeSat developers should now be able to estimate their required functional testing time on subsystem and system level at an early project stage, as a function of the targeted reliability goal for
机译:多年来,传统的卫星设计理念是由高度可靠的组件,保守设计和在子系统和集成系统级别进行广泛的性能测试的主导,以实现恶劣空间环境的长寿。 CubeSats试图选择不同的哲学,利用适当的最新的艺术品,商业储备品,如果成功,则屈服,每种小血管的每种质量数字的性能提高,风险较低,成本较低。 Cubeesats似乎承诺大学和公司在历史上更快,更好,更便宜。不幸的是,许多立方体特派团,尤其是大学内置的特派团,从未在卫星从其部署中排出后不久的可检测功能状态或失败。基于我们发达的立方体故障数据库(CFD)和其他人建议的数据,所以通过在地面上更加谨慎和充足的系统级功能测试,可以检测到大量的早期故障情况。然而,许多大学团队仍然无法计划对系统级功能测试的充足的资源,或者面对艰难的截止日期,因此无法在足够的水平上完成适当的集成系统测试,并启动永不充分奏效的卫星。使用贝叶斯方法进行新的可靠性估算工具的持续工作,以填补这一差距,并为所有开发人员提供有意义的数据,以实现可实现的可靠性和所需的立方体的功能测试时间。使用测试数据和可靠性目标来实现其实际任务,将数据与来自过去任务的统计数据和主观开发人员信仰的数据库合并,立方体开发人员现在应该能够在早期项目中估算其所需的功能测试时间和系统级别阶段,作为目标可靠性目标的函数

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