The Circular-Restricted Three-Body Problem by David Eagle

Compute and plot characteristics of the Earth-Moon-Satellite CRTBP. (aerospace, mathematics, celestial mechanics)

brent (f, x1, x2, rtol)

clpfunc(x)

crtbp_eqm (tsim, y)

orbits - plot orbits around Earth in an interactive manner. by Michael

This GUI lets you plot orbits around Earth interactively. (celestial mechanics, interactive, satellite)

orbits - plot orbits around Earth in an interactive manner

orbits(action);

Robust solver for Lambert's orbital-boundary value problem by Rody Oldenhuis

Solves any Lambert-problem robustly. Can be compiled to increase efficiency. (astrodynamics, lambert, trajectory optimizati...)

lambert(r1vec, r2vec, tf, m, muC)%#eml