MATLAB solutions of Lambert's problem

Version 1.2.0.0 (663 KB) von David Eagle
MATLAB functions and scripts for solving the geocentric and heliocentric Lambert problem.
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Aktualisiert 29. Jan 2024

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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.

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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. Abgerufen.

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Erstellt mit R2012b
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Version Veröffentlicht Versionshinweise
1.2.0.0

Updated PDF documentation and MATLAB source code.
1.1.0.0

Added main script (lambert4_64bit.m) that uses the March 17, 2014 version of SNOPT.
1.0.0.0