The following Matlab project contains the source code and Matlab examples used for keplerian state transition matrix.
Phi = keplerSTM(x0,dt,mu) will return the state transition matrix Phi
for a set of objects described by initial positions and velocities (x0)
with gravitational parameters mu, propogated along Keplerian orbits for
time dt.

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 Name | Size |
---|---|

keplerSTM.m | 4300 |

license.txt | 1316 |