Orbital Elements
Overview
The classical Keplerian orbital elements are $[a, e, i Ω, ω, ν]$. While these are the most well-known and commonly used in the astrodynamics community, they are not the only way to describe an orbit. We are also working on including two-line elements and Delaunay variables.
Functions
ThreeBodyProblem.AP2a — FunctionAP2a(rA, rP)Compute the semimajor axis given apoapsis and periapsis distances rA and rP.
ThreeBodyProblem.findrP — Functioncomputeq(rv::Array,p::Array)computeq