KeplerianOrbit

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total15 of 3,55799%4 of 8495%41063525061
KeplerianOrbit(double, double, double, double, double, double, double, double, double, double, double, double, PositionAngleType, Frame, AbsoluteDate, double)1021795%22090%21425101
addKeplerContribution(PositionAngleType, double, double[])9094%1375%1411501
computeJacobianMeanWrtCartesianElliptical()633100%n/a0107601
computeJacobianMeanWrtCartesianHyperbolic()620100%n/a0108901
KeplerianOrbit(TimeStampedPVCoordinates, Frame, double, boolean)405100%6100%0405801
computePVWithoutA()193100%4100%0303201
nonKeplerianAcceleration()180100%n/a010701
shiftedBy(double)102100%2100%0201501
initPosition()98100%2100%0201401
referenceAxes()89100%n/a0101401
computeJacobianTrueWrtCartesianHyperbolic()76100%2100%0201501
computeJacobianTrueWrtCartesianElliptical()73100%2100%0201301
computeJacobianEccentricWrtCartesianHyperbolic()53100%2100%0201001
computeJacobianEccentricWrtCartesianElliptical()50100%2100%020801
initPVCoordinates()45100%2100%020601
toString()45100%n/a010801
getHxDot()42100%2100%020501
getHyDot()42100%2100%020501
getEccentricAnomalyDot()35100%2100%020601
getMeanAnomalyDot()35100%2100%020601
checkParameterRangeInclusive(String, double, double, double)35100%1375%130401
getEquinoctialExDot()27100%n/a010301
getEquinoctialEyDot()27100%n/a010301
removeRates()27100%n/a010301
getHx()20100%2100%020301
getHy()20100%2100%020301
KeplerianOrbit(double, double, double, double, double, double, PositionAngleType, Frame, AbsoluteDate, double)19100%n/a010201
getEccentricAnomaly()17100%2100%020301
getMeanAnomaly()17100%2100%020301
getAnomaly(PositionAngleType)15100%4100%030301
getAnomalyDot(PositionAngleType)15100%4100%030301
KeplerianOrbit(Orbit)11100%n/a010201
KeplerianOrbit(PVCoordinates, Frame, AbsoluteDate, double)10100%n/a010201
getEquinoctialEx()10100%n/a010101
getEquinoctialEy()10100%n/a010101
KeplerianOrbit(TimeStampedPVCoordinates, Frame, double)9100%n/a010201
getLv()9100%n/a010101
getLvDot()9100%n/a010101
getLE()9100%n/a010101
getLEDot()9100%n/a010101
getLM()9100%n/a010101
getLMDot()9100%n/a010101
computeJacobianMeanWrtCartesian()9100%2100%020301
computeJacobianEccentricWrtCartesian()9100%2100%020301
computeJacobianTrueWrtCartesian()9100%2100%020301
writeReplace()6100%n/a010101
getA()100%n/a010101
getADot()100%n/a010101
getE()100%n/a010101
getEDot()100%n/a010101
getI()100%n/a010101
getIDot()100%n/a010101
getPerigeeArgument()100%n/a010101
getPerigeeArgumentDot()100%n/a010101
getRightAscensionOfAscendingNode()100%n/a010101
getRightAscensionOfAscendingNodeDot()100%n/a010101
getTrueAnomaly()100%n/a010101
getTrueAnomalyDot()100%n/a010101
hasRates()100%n/a010101
getType()100%n/a010101
getCachedPositionAngleType()100%n/a010101