A matlab script for designing low thrust spiral trajectories with constant periapsis radius

The following Matlab project contains the source code and Matlab examples used for a matlab script for designing low thrust spiral trajectories with constant periapsis radius. This document describes a MATLAB script named demo_lts that can be used to design and analyze a low-thrust spiral trajectory with a constant periapsis radius.

The source code and files included in this project are listed in the project files section, please make sure whether the listed source code meet your needs there.

Project Files: 

File NameSize
atan3.m 534
demo_lts.m 7166
demo_lts.pdf 742255
ecc_event.m 494
eci2mee.m 1685
eci2orb1.m 2248
license.txt 1311
mee2eci.m 1603
mee2eci_lts.m 1916
meeeqm1_lts.m 3115
meeeqm_lts.m 2937
oeprint1.m 1709
om_constants.m 523
orb2eci.m 1615
rkf78.m 4487
svprint.m 784

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