The following Matlab project contains the source code and Matlab examples used for astrodynamics and flight mechanics functions library. .
Keplerian orbits, elliptical, parabolic, hyperbolic orbits, elements conversion. Temporal problem, mean anomaly, eccentric anomaly, true anomaly. MOID. Orbits plot. Position and velocity vectors.
Orbital maneuvers: Lambert problem solution, delta-v computation, optimal time-free orbital transfer, optimal multi flyby mission.