Propagating large orbital uncertainty with TaylorIntegration.jl
Jorge A. Pérez-Hernández, Luis Eduardo Ramírez Montoya, Luis Benet
One of the main problems in the computation of orbital predictions, is the propagation of the orbital uncertainty. This problem is relevant in a wide range of scenarios, from the design of interplanetary spacecraft trajectories, to the assessment of the hazard posed by an asteroid impacting the Earth. In this talk, we present a technique to propagate large sets of initial conditions in TaylorIntegration.jl via a technique called Automatic Domain Splitting (ADS).
Aerospace Minisymposium
While Loop (4.2)