Updated 12 Dec 2019
PDF document and MATLAB script that demonstrates how to solve the Earth orbit, J2-perturbed form of Lambert’s problem. Lambert’s problem is concerned with the determination of an orbit that passes between two positions within a specified time-of-flight. This classic astrodynamic problem is also known as the orbital two-point boundary value problem (TPBVP) or the flyby and rendezvous problems.
David Eagle (2021). Gravity-perturbed Earth Orbit Lambert Problem - OTB (https://www.mathworks.com/matlabcentral/fileexchange/73662-gravity-perturbed-earth-orbit-lambert-problem-otb), MATLAB Central File Exchange. Retrieved .
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