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arXiv 2607.03424eess.SYcs.SY
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一种用于航天飞行中随机非线性问题的高效非高斯机会约束方法

An Efficient Non-Gaussian Chance Constraint Method for Stochastic Nonlinear Problems in Spaceflight

University of Texas at Austin(德克萨斯大学奥斯汀分校);Politecnico di Milano(米兰理工大学)

Ethan R. Burnett, Spencer Boone, Niccolo Michelotti

AI总结:

研究航天飞行随机非线性问题,核心方法是将真实置信轮廓视为协方差预测值的扰动并由高阶统计矩推导扰动边界几何,贡献是能对置信轮廓简单参数化并用于航天器机动目标问题。

摘要:

标准机会约束航天器制导通常依赖于飞行器状态不确定性服从高斯统计的假设。在诸如地月环境或深空飞越等前沿应用中,动力学可能特别非线性,测量间隔时间可能很长,导致需要做出结果产生非高斯分布的决策。本文展示了一种用于此类应用中随机制导的非高斯置信边界技术。我们的方法是将真实置信轮廓视为从协方差预测的轮廓的扰动,然后从计算出的高阶统计矩推导出扰动边界几何。将此技术应用于轨道力学问题中发现的所谓“香蕉形分布”,能够使用偏斜和峰度张量对置信轮廓进行简单参数化。然后将此参数化应用于随机和非线性脉冲航天器机动目标问题,并对相关非凸约束进行特殊处理。

英文摘要:

Standard chance-constrained spacecraft guidance typically relies on the assumption that uncertainties in vehicle states obey Gaussian statistics. In frontier applications such as the cislunar environment or deep space flybys, the dynamics can be particularly nonlinear, and time between measurements can be long, leading to the need to make decisions whose outcomes produce non-Gaussian distributions. This paper demonstrates a non-Gaussian confidence boundary technique for stochastic guidance in such applications. Our approach is to consider the true confidence contour as a perturbation of the one predicted from covariance, then to derive perturbed boundary geometry from computed higher-order statistical moments. Applying this technique to so-called "banana-shaped distributions", found in orbital mechanics problems, enables a simple parameterization of the confidence contour using the skew and kurtosis tensors. This parameterization is then applied to a stochastic and nonlinear impulsive spacecraft maneuver targeting problem, with special treatment of a relevant non-convex constraint.

机构、总结、中文摘要均由AI分析而来,可能存在错误,请以论文正文为准。

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