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Lambert's Problem

version 1.1.0.0 (587 KB) by David Eagle
MATLAB functions and scripts for solving the geocentric and heliocentric Lambert problem.

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Updated 10 Jul 2014

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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.

Comments and Ratings (9)

Youl find the algorithms for orb2eci algorithm and source code at the R.H Gooding paper
http://adsabs.harvard.edu/full/1986CeMec..38..307O

PAUL GILLES

Sulav

Hello,

Can you give some references for the algorithm you have programmed in orb2eci file?

Guanwei He

sun Chong

Abel

Updates

1.1.0.0

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

MATLAB Release Compatibility
Created with R2012b
Compatible with any release
Platform Compatibility
Windows macOS Linux