PDF document and four MATLAB scripts that demonstrate how to solve the Earth orbit, interplanetary, and 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). Lambert's Problem (https://www.mathworks.com/matlabcentral/fileexchange/39530-lambert-s-problem), MATLAB Central File Exchange. Retrieved .
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