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Uncertainty optimization applied to the Monte Carlo analysis of planetary entry trajectories.

机译:不确定性优化应用于行星进入轨迹的蒙特卡洛分析。

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摘要

Future robotic missions to Mars, as well as any human missions, will require precise entries to ensure safe landings near science objectives and pre-deployed assets. Planning for these missions will depend heavily on Monte Carlo analyses to evaluate active guidance algorithms, assess the impact of off-nominal conditions, and account for uncertainty. The dependability of Monte Carlo forecasts, however, is limited by the accuracy and completeness of the assumed uncertainties. This is because Monte Carlo analysis is a forward driven problem; beginning with the input uncertainties and proceeding to the forecast output statistics. An improvement to the Monte Carlo analysis is needed that will allow the problem to be worked in reverse. In this way, the largest allowable dispersions that achieve the required mission objectives can be determined quantitatively.; This thesis proposes a methodology to optimize the uncertainties in the Monte Carlo analysis of spacecraft landing footprints. A metamodel is used to first write polynomial expressions for the size of the landing footprint as functions of the independent uncertainty extrema. The coefficients of the metamodel are determined by performing experiments. The metamodel is then used in a constrained optimization procedure to minimize a cost-tolerance function. First, a two-dimensional proof-of-concept problem was used to evaluate the feasibility of this optimization method. Next, the optimization method was further demonstrated on the Mars Surveyor Program 2001 Lander. The purpose of this example was to demonstrate that the methodology developed during the proof-of-concept could be scaled to solve larger, more complicated, “real world” problems.; This research has shown that is possible to control the size of the landing footprint and establish tolerances for mission uncertainties. A simplified metamodel was developed, which is enabling for realistic problems with more than just a few uncertainties. A confidence interval on the size of the footprint was developed, based on the assumption of a bivariate normal distribution. Because the confidence interval is a function of sample size, it may be used to determine, a priori, how many simulations must be performed to achieve a given accuracy in the size of the footprint.
机译:未来对火星的机器人飞行以及任何人类飞行都将需要精确的进入,以确保安全降落在科学目标和预先部署的资产附近。这些任务的计划将在很大程度上取决于Monte Carlo分析,以评估主动制导算法,评估非标称条件的影响并解决不确定性。但是,蒙特卡洛预测的可靠性受到假定不确定性的准确性和完整性的限制。这是因为蒙特卡洛分析是一个前驱问题。从输入不确定性开始,然后进行预测输出统计。需要对蒙特卡洛分析进行改进,以使问题可以逆向解决。这样,可以定量确定达到所需任务目标的最大允许色散。本文提出了一种方法,以优化对航天器着陆足迹的蒙特卡洛分析中的不确定性。使用元模型首先针对着陆足迹的大小编写多项式表达式,以作为独立不确定性极值的函数。通过执行实验确定元模型的系数。然后,将元模型用于约束优化过程中以最小化成本容忍功能。首先,使用二维概念验证问题来评估此优化方法的可行性。接下来,在Mars Surveyor Program 2001 Lander上进一步演示了优化方法。这个例子的目的是证明概念验证期间开发的方法可以扩展以解决更大,更复杂的“现实世界”问题。这项研究表明,可以控制着陆足迹的大小并确定任务不确定性的公差。开发了一个简化的元模型,该模型可以解决不只是几个不确定性的现实问题。基于二元正态分布的假设,建立了足迹尺寸的置信区间。因为置信区间是样本大小的函数,所以它可以用来确定必须先执行多少次模拟才能在足迹尺寸上达到给定的精度

著录项

  • 作者

    Way, David Wesley.;

  • 作者单位

    Georgia Institute of Technology.;

  • 授予单位 Georgia Institute of Technology.;
  • 学科 Engineering Aerospace.
  • 学位 Ph.D.
  • 年度 2001
  • 页码 212 p.
  • 总页数 212
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类 航空、航天技术的研究与探索;
  • 关键词

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