Stochastic analysis of impulsive thrust uncertainties in the CR3BP
Optimization and Control
2025-04-01 v1
Abstract
This paper employs an alternate dynamical model of the circular restricted three body problem to quantify uncertainties associated with spacecraft thrusting maneuvers. A non-product quadrature scheme known as Conjugate Unscented Transform (CUT) is employed to determine the higher order system sensitivities through a computationally efficient data driven approach. Moreover, the CUT scheme, in conjunction with a sparse approximation method, is used to find an analytical representation of the time evolution of the state probability density function (pdf).
Cite
@article{arxiv.2503.23628,
title = {Stochastic analysis of impulsive thrust uncertainties in the CR3BP},
author = {Sharad Sharan and Amit Jain and Roshan T. Eapen and Puneet Singla},
journal= {arXiv preprint arXiv:2503.23628},
year = {2025}
}