KeplerianOrbit(TimeStampedPVCoordinates, Frame, double, boolean) | | 97% | | 80% | 2 | 6 | 1 | 66 | 0 | 1 |
initializeCachedAnomaly(double, double, PositionAngleType) | | 95% | | 91% | 2 | 15 | 2 | 27 | 0 | 1 |
getTrueAnomalyDot() | | 94% | | 90% | 1 | 7 | 1 | 17 | 0 | 1 |
getEccentricAnomalyDot() | | 94% | | 90% | 1 | 7 | 1 | 17 | 0 | 1 |
getMeanAnomalyDot() | | 94% | | 90% | 1 | 7 | 1 | 17 | 0 | 1 |
getTrueAnomaly() | | 89% | | 87% | 1 | 6 | 1 | 7 | 0 | 1 |
getEccentricAnomaly() | | 89% | | 87% | 1 | 6 | 1 | 7 | 0 | 1 |
getMeanAnomaly() | | 89% | | 87% | 1 | 6 | 1 | 7 | 0 | 1 |
computeJacobianMeanWrtCartesianElliptical() | | 100% | | n/a | 0 | 1 | 0 | 76 | 0 | 1 |
computeJacobianMeanWrtCartesianHyperbolic() | | 100% | | n/a | 0 | 1 | 0 | 89 | 0 | 1 |
computePVWithoutA() | | 100% | | 100% | 0 | 3 | 0 | 32 | 0 | 1 |
nonKeplerianAcceleration() | | 100% | | n/a | 0 | 1 | 0 | 7 | 0 | 1 |
KeplerianOrbit(double, double, double, double, double, double, double, double, double, double, double, double, PositionAngleType, PositionAngleType, Frame, AbsoluteDate, double) | | 100% | | 100% | 0 | 5 | 0 | 30 | 0 | 1 |
shiftedBy(TimeOffset) | | 100% | | 100% | 0 | 2 | 0 | 15 | 0 | 1 |
initPosition() | | 100% | | 100% | 0 | 2 | 0 | 14 | 0 | 1 |
referenceAxes() | | 100% | | n/a | 0 | 1 | 0 | 14 | 0 | 1 |
computeJacobianTrueWrtCartesianHyperbolic() | | 100% | | 100% | 0 | 2 | 0 | 15 | 0 | 1 |
computeJacobianTrueWrtCartesianElliptical() | | 100% | | 100% | 0 | 2 | 0 | 13 | 0 | 1 |
computeJacobianEccentricWrtCartesianHyperbolic() | | 100% | | 100% | 0 | 2 | 0 | 10 | 0 | 1 |
computeKeplerianAnomalyDot(PositionAngleType, double, double, double, double, PositionAngleType) | | 100% | | 100% | 0 | 3 | 0 | 9 | 0 | 1 |
computeJacobianEccentricWrtCartesianElliptical() | | 100% | | 100% | 0 | 2 | 0 | 8 | 0 | 1 |
initPVCoordinates() | | 100% | | 100% | 0 | 2 | 0 | 7 | 0 | 1 |
toString() | | 100% | | n/a | 0 | 1 | 0 | 8 | 0 | 1 |
getHxDot() | | 100% | | 100% | 0 | 2 | 0 | 5 | 0 | 1 |
getHyDot() | | 100% | | 100% | 0 | 2 | 0 | 5 | 0 | 1 |
checkParameterRangeInclusive(String, double, double, double) | | 100% | | 75% | 1 | 3 | 0 | 4 | 0 | 1 |
getEquinoctialExDot() | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
getEquinoctialEyDot() | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
removeRates() | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
KeplerianOrbit(double, double, double, double, double, double, PositionAngleType, PositionAngleType, Frame, AbsoluteDate, double) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
KeplerianOrbit(double, double, double, double, double, double, double, double, double, double, double, double, PositionAngleType, Frame, AbsoluteDate, double) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
getHx() | | 100% | | 100% | 0 | 2 | 0 | 3 | 0 | 1 |
getHy() | | 100% | | 100% | 0 | 2 | 0 | 3 | 0 | 1 |
addKeplerContribution(PositionAngleType, double, double[]) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
getAnomaly(PositionAngleType) | | 100% | | 100% | 0 | 3 | 0 | 3 | 0 | 1 |
getAnomalyDot(PositionAngleType) | | 100% | | 100% | 0 | 3 | 0 | 3 | 0 | 1 |
KeplerianOrbit(double, double, double, double, double, double, PositionAngleType, Frame, AbsoluteDate, double) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
KeplerianOrbit(Orbit) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
KeplerianOrbit(PVCoordinates, Frame, AbsoluteDate, double) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
getEquinoctialEx() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getEquinoctialEy() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
KeplerianOrbit(TimeStampedPVCoordinates, Frame, double) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
getLv() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getLvDot() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getLE() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getLEDot() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getLM() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getLMDot() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
computeJacobianMeanWrtCartesian() | | 100% | | 100% | 0 | 2 | 0 | 3 | 0 | 1 |
computeJacobianEccentricWrtCartesian() | | 100% | | 100% | 0 | 2 | 0 | 3 | 0 | 1 |
computeJacobianTrueWrtCartesian() | | 100% | | 100% | 0 | 2 | 0 | 3 | 0 | 1 |
initializeCachedAnomaly(double, PositionAngleType) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
shiftedBy(double) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
writeReplace() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getA() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getADot() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getE() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getEDot() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getI() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getIDot() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getPerigeeArgument() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getPerigeeArgumentDot() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getRightAscensionOfAscendingNode() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getRightAscensionOfAscendingNodeDot() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getCachedPositionAngleType() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
hasRates() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getType() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |