Gravity-perturbed Earth Orbit Lambert Problem - OTB

Version 1.0.0 (560 ko) par David Eagle
Optimization Toolbox version of the lambert4.m MATLAB script which solves the gravity-perturbed Lambert problem
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Mise à jour 12 déc. 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.

Citation pour cette source

David Eagle (2024). 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. Récupéré le .

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Créé avec R2019b
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Version Publié le Notes de version
1.0.0