The following Matlab project contains the source code and Matlab examples used for circular orbit plane change.
This document presents the geometry and equations associated with the single impulse maneuver that modifies the inclination and/or right ascension of the ascending node (RAAN) of circular orbits.

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 |
---|---|

atan3.m | 532 |

getoe.m | 3689 |

license.txt | 1311 |

maneuver1.m | 7832 |

om_constants.m | 800 |

orb2eci.m | 1615 |

plane_change.pdf | 236526 |

twobody2.m | 2755 |

ueci2angles.m | 943 |