getHasManeuver() | | 88% | | 50% | 1 | 2 | 0 | 1 | 0 | 1 |
generateKeplerianOrbit() | | 100% | | 100% | 0 | 2 | 0 | 5 | 0 | 1 |
getSatelliteCoordinates(String) | | 100% | | 100% | 0 | 2 | 0 | 3 | 0 | 1 |
generateCartesianOrbit() | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
OPMFile() | | 100% | | n/a | 0 | 1 | 0 | 4 | 0 | 1 |
getSatelliteCoordinatesOPM() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getPVCoordinates() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
generateSpacecraftState() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getManeuver(int) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
addManeuver(OPMFile.Maneuver) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
getCoordinateSystem() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
setPosition(Vector3D) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
setVelocity(Vector3D) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
getNbManeuvers() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getManeuvers() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getMetaDataComment() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getTimeSystem() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getMetaData() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getPosition() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getVelocity() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |