checkConsistency(AbsolutePVCoordinates, Attitude) | | 29% | | 50% | 2 | 3 | 5 | 8 | 0 | 1 |
toString() | | 0% | | n/a | 1 | 1 | 1 | 1 | 1 | 1 |
SpacecraftState(AbsolutePVCoordinates, double) | | 0% | | n/a | 1 | 1 | 3 | 3 | 1 | 1 |
getAbsPVA() | | 46% | | 50% | 1 | 2 | 1 | 3 | 0 | 1 |
getOrbit() | | 46% | | 50% | 1 | 2 | 1 | 3 | 0 | 1 |
getPosition(Frame) | | 69% | | 50% | 1 | 2 | 0 | 1 | 0 | 1 |
getPVCoordinates(Frame) | | 69% | | 50% | 1 | 2 | 0 | 1 | 0 | 1 |
ensureCompatibleAdditionalStates(SpacecraftState) | | 98% | | 83% | 4 | 13 | 2 | 31 | 0 | 1 |
getA() | | 88% | | 50% | 1 | 2 | 0 | 1 | 0 | 1 |
getEquinoctialEx() | | 88% | | 50% | 1 | 2 | 0 | 1 | 0 | 1 |
getEquinoctialEy() | | 88% | | 50% | 1 | 2 | 0 | 1 | 0 | 1 |
getE() | | 88% | | 50% | 1 | 2 | 0 | 1 | 0 | 1 |
checkConsistency(Orbit, Attitude) | | 100% | | 100% | 0 | 3 | 0 | 8 | 0 | 1 |
SpacecraftState(AbsolutePVCoordinates, Attitude, double, DoubleArrayDictionary, DoubleArrayDictionary) | | 100% | | 100% | 0 | 3 | 0 | 13 | 0 | 1 |
SpacecraftState(Orbit, Attitude, double, DoubleArrayDictionary, DoubleArrayDictionary) | | 100% | | 100% | 0 | 3 | 0 | 13 | 0 | 1 |
addAdditionalState(String, double[]) | | 100% | | 100% | 0 | 2 | 0 | 5 | 0 | 1 |
addAdditionalStateDerivative(String, double[]) | | 100% | | 100% | 0 | 2 | 0 | 5 | 0 | 1 |
shiftedBy(double) | | 100% | | 100% | 0 | 2 | 0 | 5 | 0 | 1 |
shiftAdditional(double) | | 100% | | 100% | 0 | 4 | 0 | 9 | 0 | 1 |
getAdditionalState(String) | | 100% | | 100% | 0 | 2 | 0 | 4 | 0 | 1 |
getAdditionalStateDerivative(String) | | 100% | | 100% | 0 | 2 | 0 | 4 | 0 | 1 |
SpacecraftState(Orbit) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
SpacecraftState(Orbit, double) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
SpacecraftState(AbsolutePVCoordinates) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
SpacecraftState(Orbit, DoubleArrayDictionary) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
SpacecraftState(Orbit, double, DoubleArrayDictionary) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
SpacecraftState(AbsolutePVCoordinates, DoubleArrayDictionary) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
SpacecraftState(AbsolutePVCoordinates, double, DoubleArrayDictionary) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
writeReplace() | | 100% | | 100% | 0 | 2 | 0 | 1 | 0 | 1 |
toTransform() | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
getDate() | | 100% | | 100% | 0 | 2 | 0 | 1 | 0 | 1 |
getFrame() | | 100% | | 100% | 0 | 2 | 0 | 1 | 0 | 1 |
getPosition() | | 100% | | 100% | 0 | 2 | 0 | 1 | 0 | 1 |
getPVCoordinates() | | 100% | | 100% | 0 | 2 | 0 | 1 | 0 | 1 |
toStaticTransform() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
hasAdditionalState(String) | | 100% | | 100% | 0 | 2 | 0 | 1 | 0 | 1 |
hasAdditionalStateDerivative(String) | | 100% | | 100% | 0 | 2 | 0 | 1 | 0 | 1 |
getMu() | | 100% | | 100% | 0 | 2 | 0 | 1 | 0 | 1 |
getKeplerianPeriod() | | 100% | | 100% | 0 | 2 | 0 | 1 | 0 | 1 |
getKeplerianMeanMotion() | | 100% | | 100% | 0 | 2 | 0 | 1 | 0 | 1 |
getHx() | | 100% | | 100% | 0 | 2 | 0 | 1 | 0 | 1 |
getHy() | | 100% | | 100% | 0 | 2 | 0 | 1 | 0 | 1 |
getLv() | | 100% | | 100% | 0 | 2 | 0 | 1 | 0 | 1 |
getLE() | | 100% | | 100% | 0 | 2 | 0 | 1 | 0 | 1 |
getLM() | | 100% | | 100% | 0 | 2 | 0 | 1 | 0 | 1 |
getI() | | 100% | | 100% | 0 | 2 | 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, double, DoubleArrayDictionary) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
SpacecraftState(AbsolutePVCoordinates, Attitude) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
SpacecraftState(AbsolutePVCoordinates, Attitude, double) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
SpacecraftState(AbsolutePVCoordinates, Attitude, double, DoubleArrayDictionary) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
SpacecraftState(Orbit, Attitude, DoubleArrayDictionary) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
SpacecraftState(AbsolutePVCoordinates, Attitude, DoubleArrayDictionary) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
isOrbitDefined() | | 100% | | 100% | 0 | 2 | 0 | 1 | 0 | 1 |
getDefaultAttitudeProvider(Frame) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getAdditionalStatesValues() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getAdditionalStatesDerivatives() | | 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 |