Orbit Uncertainty Propagation and Sensitivity Analysis With Separated Representations
Marc Balducci, Brandon Jones, Alireza Doostan

TL;DR
This paper introduces a separated representation method for orbit uncertainty propagation that reduces computational costs and handles high-dimensional, non-Gaussian inputs effectively, demonstrated through satellite case studies.
Contribution
It presents a novel application of separated representations for orbit uncertainty propagation, enabling linear scaling with input dimension and improved tractability over traditional methods.
Findings
Accurately propagates orbit uncertainty with up to 20 inputs.
Linear computational cost with respect to sample size.
Effective sensitivity analysis of uncertain inputs.
Abstract
Most approximations for stochastic differential equations with high-dimensional, non-Gaussian inputs suffer from a rapid (e.g., exponential) increase of computational cost, an issue known as the curse of dimensionality. In astrodynamics, this results in reduced accuracy when propagating an orbit-state probability density function. This paper considers the application of separated representations for orbit uncertainty propagation, where future states are expanded into a sum of products of univariate functions of initial states and other uncertain parameters. An accurate generation of separated representation requires a number of state samples that is linear in the dimension of input uncertainties. The computation cost of a separated representation scales linearly with respect to the sample count, thereby improving tractability when compared to methods that suffer from the curse of…
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