arXiv:2607.16914cs.ROcs.IT2026-07

用相对熵约束提升非线性系统轨迹规划的鲁棒性

Approximate Relative Entropy Constraints for Nonlinear Covariance Steering Under Distribution Ambiguity

论文配图:Approximate Relative Entropy Constraints for Nonlinear Covariance Steering Under Distribution Ambiguity
图 1 · 摘自论文原文
  • 基于相对熵构建分布鲁棒的协方差引导框架
  • 可计算风险敏感指标的上界,控制分布偏差
  • 适合高精度航天器轨迹设计等安全关键场景

协方差引导为设计线性随机反馈策略提供了高效框架,但其扩展到非线性系统依赖于通过局部线性化获得的高斯近似。由于该近似与真实非线性状态分布可能存在显著差异,碰撞概率、均方误差等风险敏感量的估计可能不准确。本文基于相对熵(即Kullback-Leibler散度,KLD)构建了分布鲁棒的协方差引导框架,以处理传播概率密度函数中的不确定性。利用指数积分的变分表示,推导出在KLD模糊集上风险敏感量的可计算上界。进一步建立真值分布与高斯参考近似之间KLD时间变化率的上界,并在一定假设下,使其受协方差引导优化变量控制。将这些约束纳入序列凸规划算法中,设计出使真实分布保持贴近高斯近似的同时,满足风险敏感性能约束的随机引导策略。该方法在两个近似直线晕轨道间的复杂非线性航天器转移任务中得到验证。

原文摘要 · Abstract (English)

Covariance steering provides an efficient framework for designing linear stochastic feedback policies, but its extension to nonlinear systems relies on a Gaussian surrogate obtained through local linearization. Because this surrogate may differ substantially from the true nonlinear state distribution, risk-sensitive quantities such as collision probability and mean-squared error may be inaccurately estimated. This work develops a distributionally robust covariance-steering framework based on the relative entropy, also known as the Kullback-Leibler divergence (KLD), to account for ambiguity in the propagated probability density function. Using a variational representation of exponential integrals, we derive computable upper bounds on risk-sensitive quantities over a KLD ambiguity set. We then formulate an upper bound on the time rate of change of the KLD between the true nonlinear distribution and a Gaussian reference surrogate. Under some assumptions, this bound is controlled by decision variables within a covariance-steering formulation. The resulting constraints are incorporated into a sequential convex programming algorithm to design stochastic guidance policies that keep the true distribution close to its Gaussian surrogate while enforcing bounds on risk-sensitive performance measures. The proposed approach is demonstrated on a challenging nonlinear spacecraft transfer between two near-rectilinear halo orbits.

协方差引导相对熵鲁棒控制航天任务

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