arXiv · 2503.23628
Stochastic analysis of impulsive thrust uncertainties in the CR3BP
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).
Explore related subjects
Keep this discovery
Explore connections, maps & timelines
Sharad Sharan, Amit Jain, Roshan T. Eapen, Puneet Singla. 2025-03-30. Stochastic analysis of impulsive thrust uncertainties in the CR3BP. https://arxiv.org/abs/2503.23628
Cite the original work for its findings. Save a collection to share your selection of sources.