KeplerianOrbit

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total45 of 3,95698%11 of 14492%111479594067
KeplerianOrbit(TimeStampedPVCoordinates, Frame, double, boolean)942297%2880%2616601
initializeCachedAnomaly(double, double, PositionAngleType)611995%22291%21522701
getTrueAnomalyDot()8294%1990%1711701
getEccentricAnomalyDot()8294%1990%1711701
getMeanAnomalyDot()8294%1990%1711701
getTrueAnomaly()4389%1787%161701
getEccentricAnomaly()4389%1787%161701
getMeanAnomaly()4389%1787%161701
computeJacobianMeanWrtCartesianElliptical()633100%n/a0107601
computeJacobianMeanWrtCartesianHyperbolic()620100%n/a0108901
computePVWithoutA()193100%4100%0303201
nonKeplerianAcceleration()180100%n/a010701
KeplerianOrbit(double, double, double, double, double, double, double, double, double, double, double, double, PositionAngleType, PositionAngleType, Frame, AbsoluteDate, double)148100%8100%0503001
shiftedBy(TimeOffset)107100%2100%0201501
initPosition()98100%2100%0201401
referenceAxes()89100%n/a0101401
computeJacobianTrueWrtCartesianHyperbolic()76100%2100%0201501
computeJacobianTrueWrtCartesianElliptical()73100%2100%0201301
computeJacobianEccentricWrtCartesianHyperbolic()53100%2100%0201001
computeKeplerianAnomalyDot(PositionAngleType, double, double, double, double, PositionAngleType)53100%4100%030901
computeJacobianEccentricWrtCartesianElliptical()50100%2100%020801
initPVCoordinates()45100%2100%020701
toString()45100%n/a010801
getHxDot()42100%2100%020501
getHyDot()42100%2100%020501
checkParameterRangeInclusive(String, double, double, double)35100%1375%130401
getEquinoctialExDot()27100%n/a010301
getEquinoctialEyDot()27100%n/a010301
removeRates()27100%n/a010301
KeplerianOrbit(double, double, double, double, double, double, PositionAngleType, PositionAngleType, Frame, AbsoluteDate, double)20100%n/a010201
KeplerianOrbit(double, double, double, double, double, double, double, double, double, double, double, double, PositionAngleType, Frame, AbsoluteDate, double)20100%n/a010201
getHx()20100%2100%020301
getHy()20100%2100%020301
addKeplerContribution(PositionAngleType, double, double[])18100%n/a010201
getAnomaly(PositionAngleType)15100%4100%030301
getAnomalyDot(PositionAngleType)15100%4100%030301
KeplerianOrbit(double, double, double, double, double, double, PositionAngleType, Frame, AbsoluteDate, double)14100%n/a010201
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
initializeCachedAnomaly(double, PositionAngleType)8100%n/a010101
shiftedBy(double)7100%n/a010101
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
getCachedPositionAngleType()100%n/a010101
hasRates()100%n/a010101
getType()100%n/a010101