Element | Missed Instructions | Cov. | Missed Branches | Cov. | Missed | Cxty | Missed | Lines | Missed | Methods |
Total | 1 of 137 | 99% | 1 of 4 | 75% | 1 | 18 | 0 | 27 | 0 | 16 |
getHasManeuver() | ![]() ![]() | 87% | ![]() ![]() | 50% | 1 | 2 | 0 | 1 | 0 | 1 |
generateKeplerianOrbit() | ![]() | 100% | ![]() | 100% | 0 | 2 | 0 | 5 | 0 | 1 |
generateCartesianOrbit() | ![]() | 100% | n/a | 0 | 1 | 0 | 2 | 0 | 1 | |
OPMFile() | ![]() | 100% | n/a | 0 | 1 | 0 | 4 | 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 | |
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 | |
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 |