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Modeling Martian planetary entry descent and landing using Monte Carlo driven response surface methodology.

机译:使用蒙特卡洛驱动的响应面方法对火星行星入口下降和着陆进行建模。

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摘要

Response surface methodology (RSM) is a statistical method that explores the relationships between several descriptive variables and one or more response variables. For over sixty years, among other areas, it has been utilized in quality engineering, process engineering, aircraft engineering, economics, chemical engineering, automotive engineering and design/technique optimization. In this dissertation, RSM is utilized to produce regression models that represent the planetary entry, descent and landing (EDL) process. A complete understanding of EDL process is an essential component of any planetary exploration. Research in this area is ongoing and confidence in the ability to explore known celestial bodies is growing. The purpose of this research was to develop a unique technique for modeling EDL scenarios based on an understanding of the Martian atmosphere and the Viking Lander. A two degree of freedom trajectory simulation was developed for a Martian EDL. Statistical engineering was applied through formal experiment design to provide an empirical model between sixteen input variables and thirty-eight outputs pertinent to EDL. RSM was used in conjunction with the EDL simulation to develop second order regression models for each response as a function of all of the factors. The challenge comes when reducing the full quaradic model to a reduced model with the minimum amount of variables while remaining statistically sound. In this research full quadratic regression models were reduced using a technique developed during the research process called the Multiple Adjusted R-Squared Reduction (MARR) method. The MARR method is a process of reducing regression models so that their calculated Adjusted R-Squared (ARS) values are as close to a target ARS (chosen here as 0.99 +/- 0.004) as possible. Eighteen of the thirty-eight models developed met the Adjusted R-Squared target and were further used in Monte Carlo experiments to test the models dependence on the input variables and to develop EDL pertinent trade studies based on the reduced models.
机译:响应面方法(RSM)是一种统计方法,探讨了几个描述性变量与一个或多个响应变量之间的关系。六十多年来,它在质量工程,过程工程,飞机工程,经济学,化学工程,汽车工程以及设计/技术优化等领域得到广泛应用。本文利用RSM方法建立了代表行星进入,下降和着陆(EDL)过程的回归模型。全面了解EDL过程是任何行星勘探的重要组成部分。该领域的研究正在进行中,并且对探索已知天体的能力的信心正在增强。这项研究的目的是基于对火星大气层和维京人着陆器的理解,开发一种独特的技术来对EDL场景进行建模。针对火星EDL开发了两个自由度轨迹模拟。通过正式的实验设计应用了统计工程,以提供与EDL相关的16个输入变量和38个输出之间的经验模型。 RSM与EDL仿真结合使用,针对每个响应根据所有因素开发了二阶回归模型。当将完整的拟辐射模型简化为具有最小变量量同时又保持统计上合理的简化模型时,挑战就来了。在这项研究中,使用研究过程中开发的一种称为多重调整R平方缩减(MARR)方法的技术来简化整个二次回归模型。 MARR方法是减少回归模型的过程,以使它们的计算出的调整后R平方(ARS)值尽可能接近目标ARS(此处选择为0.99 +/- 0.004)。在开发的38个模型中,有18个达到了调整后R平方目标,并进一步用于蒙特卡洛实验,以测试模型对输入变量的依赖性,并基于简化模型开发EDL相关贸易研究。

著录项

  • 作者

    Norman, Narcrisha S.;

  • 作者单位

    Old Dominion University.;

  • 授予单位 Old Dominion University.;
  • 学科 Statistics.;Physics Theory.;Engineering Aerospace.
  • 学位 Ph.D.
  • 年度 2012
  • 页码 288 p.
  • 总页数 288
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类 古生物学;
  • 关键词

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