ensureCompatibleAdditionalStates(SpacecraftState) | | 99% | | 83% | 2 | 7 | 1 | 13 | 0 | 1 |
interpolate(AbsoluteDate, Collection) | | 100% | | 100% | 0 | 6 | 0 | 26 | 0 | 1 |
checkConsistency(Orbit, Attitude) | | 100% | | 100% | 0 | 3 | 0 | 5 | 0 | 1 |
SpacecraftState(Orbit, Attitude, double, Map) | | 100% | | 100% | 0 | 3 | 0 | 12 | 0 | 1 |
addAdditionalState(String, double[]) | | 100% | | n/a | 0 | 1 | 0 | 4 | 0 | 1 |
getAdditionalState(String) | | 100% | | 100% | 0 | 2 | 0 | 3 | 0 | 1 |
toTransform() | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
SpacecraftState(Orbit) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
SpacecraftState(Orbit, double) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
SpacecraftState(Orbit, Map) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
SpacecraftState(Orbit, double, Map) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
shiftedBy(double) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
SpacecraftState(Orbit, Attitude) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
SpacecraftState(Orbit, Attitude, double) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
SpacecraftState(Orbit, Attitude, Map) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
writeReplace() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
hasAdditionalState(String) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getPVCoordinates(Frame) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getDate() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getFrame() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getAdditionalStates() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getMu() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getKeplerianPeriod() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getKeplerianMeanMotion() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getA() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getEquinoctialEx() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getEquinoctialEy() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getHx() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getHy() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getLv() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getLE() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getLM() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getE() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getI() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getPVCoordinates() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getOrbit() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getAttitude() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getMass() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |