OrbitalTrajectories.jl is a modern orbital trajectory design, optimisation, and analysis library for Julia, providing methods and tools for designing spacecraft orbits and transfers via high-performance simulations of astrodynamical models.
This is a development release that is not registered with the Julia General registry. It provides initial support for N-order State Transition Tensors, including automatic Symbolic Variational Equations (currently up to 2nd-order) and Automatic Differentiation (tested up to 3rd-order) for any astrodynamical model.
Note that this release does not pass current CI as there are numerous breaking changes in the interface, but has been locally tested on some simpler applications.
Changes: