KeplerianOrbit

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total27 of 4,21599%6 of 12295%61315623067
meanToHyperbolicEccentric(double, double)1211590%21487%2922301
KeplerianOrbit(double, double, double, double, double, double, double, double, double, double, double, double, PositionAngle, Frame, AbsoluteDate, double)1022595%22090%21425101
addKeplerContribution(PositionAngle, double, double[])9094%1375%1411501
computeJacobianMeanWrtCartesianElliptical()629100%n/a0107401
computeJacobianMeanWrtCartesianHyperbolic()618100%n/a0108801
KeplerianOrbit(TimeStampedPVCoordinates, Frame, double, boolean)411100%6100%0405801
interpolate(AbsoluteDate, Stream)296100%12100%0704401
computePVWithoutA()249100%4100%0304201
meanToEllipticEccentric(double, double)195100%10100%0602601
nonKeplerianAcceleration()180100%n/a010701
shiftedBy(double)102100%2100%0201501
computeJacobianTrueWrtCartesianElliptical()76100%2100%0201501
computeJacobianTrueWrtCartesianHyperbolic()76100%2100%0201501
computeJacobianEccentricWrtCartesianElliptical()53100%2100%0201001
computeJacobianEccentricWrtCartesianHyperbolic()53100%2100%0201001
eMeSinE(double, double)47100%2100%0201001
initPVCoordinates()45100%2100%020601
toString()45100%n/a010801
getHxDot()44100%2100%020601
getHyDot()44100%2100%020601
getMeanAnomalyDot()39100%2100%020601
getEccentricAnomalyDot()35100%2100%020601
checkParameterRangeInclusive(String, double, double, double)35100%1375%130401
ellipticEccentricToTrue(double, double)30100%n/a010201
trueToEllipticEccentric(double, double)28100%n/a010201
getEquinoctialExDot()28100%n/a010401
getEquinoctialEyDot()28100%n/a010401
getMeanAnomaly()23100%2100%020301
trueToHyperbolicEccentric(double, double)20100%n/a010201
getHx()20100%2100%020301
getHy()20100%2100%020301
KeplerianOrbit(double, double, double, double, double, double, PositionAngle, Frame, AbsoluteDate, double)19100%n/a010201
getEccentricAnomaly()17100%2100%020101
hyperbolicEccentricToTrue(double, double)17100%n/a010101
getAnomaly(PositionAngle)15100%4100%030301
getAnomalyDot(PositionAngle)15100%4100%030301
KeplerianOrbit(Orbit)11100%n/a010201
computeJacobianMeanWrtCartesian()11100%2100%020301
computeJacobianEccentricWrtCartesian()11100%2100%020301
computeJacobianTrueWrtCartesian()11100%2100%020301
static {...}11100%n/a010601
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
ellipticEccentricToMean(double, double)7100%n/a010101
hyperbolicEccentricToMean(double, 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
getTrueAnomaly()100%n/a010101
getTrueAnomalyDot()100%n/a010101
getType()100%n/a010101