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Gravity-perturbed Earth Orbit Lambert Problem - OTB

version 1.0.0 (560 KB) by David Eagle
Optimization Toolbox version of the lambert4.m MATLAB script which solves the gravity-perturbed Lambert problem


Updated 12 Dec 2019

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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.

Cite As

David Eagle (2021). Gravity-perturbed Earth Orbit Lambert Problem - OTB (, MATLAB Central File Exchange. Retrieved .

MATLAB Release Compatibility
Created with R2019b
Compatible with any release
Platform Compatibility
Windows macOS Linux

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