Gravity-perturbed Earth Orbit Lambert Problem - OTB
Optimization Toolbox version of the lambert4.m MATLAB script which solves the gravity-perturbed Lambert problem
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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 (2026). 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 .
General Information
- Version 1.0.0 (560 KB)
MATLAB Release Compatibility
- Compatible with any release
Platform Compatibility
- Windows
- macOS
- Linux
| Version | Published | Release Notes | Action |
|---|---|---|---|
| 1.0.0 |
