MATLAB solutions of Lambert's problem
Version 1.2.0.0 (663 ko) par
David Eagle
MATLAB functions and scripts for solving the geocentric and heliocentric Lambert problem.
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.
Citation pour cette source
David Eagle (2024). MATLAB solutions of Lambert's problem (https://www.mathworks.com/matlabcentral/fileexchange/39530-matlab-solutions-of-lambert-s-problem), MATLAB Central File Exchange. Récupéré le .
Compatibilité avec les versions de MATLAB
Créé avec
R2012b
Compatible avec toutes les versions
Plateformes compatibles
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Version | Publié le | Notes de version | |
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1.2.0.0 | Updated PDF documentation and MATLAB source code. |
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1.1.0.0 | Added main script (lambert4_64bit.m) that uses the March 17, 2014 version of SNOPT. |
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1.0.0.0 |