FieldKeplerianOrbit

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total27 of 5,15399%6 of 14695%61455692069
meanToHyperbolicEccentric(CalculusFieldElement, CalculusFieldElement)1214792%21487%2922401
FieldKeplerianOrbit(CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, PositionAngle, Frame, FieldAbsoluteDate, CalculusFieldElement)1026296%22090%21425401
addKeplerContribution(PositionAngle, CalculusFieldElement, CalculusFieldElement[])11995%1375%1411501
computeJacobianMeanWrtCartesianElliptical()778100%n/a0108601
computeJacobianMeanWrtCartesianHyperbolic()749100%n/a0108901
FieldKeplerianOrbit(TimeStampedFieldPVCoordinates, Frame, CalculusFieldElement, boolean)492100%6100%0406201
computePVWithoutA()301100%4100%0304201
interpolate(FieldAbsoluteDate, Stream)298100%12100%0704701
meanToEllipticEccentric(CalculusFieldElement, CalculusFieldElement)271100%12100%0703001
nonKeplerianAcceleration()203100%n/a0102201
shiftedBy(CalculusFieldElement)114100%2100%0201601
computeJacobianTrueWrtCartesianElliptical()89100%2100%0201301
computeJacobianTrueWrtCartesianHyperbolic()88100%2100%0201501
toOrbit()83100%2100%020901
eMeSinE(CalculusFieldElement, CalculusFieldElement)63100%2100%0201001
computeJacobianEccentricWrtCartesianHyperbolic()58100%2100%0201001
computeJacobianEccentricWrtCartesianElliptical()57100%2100%020801
toString()51100%n/a010801
getHxDot()49100%4100%030701
getHyDot()49100%4100%030701
initPVCoordinates()49100%2100%020701
ellipticEccentricToTrue(CalculusFieldElement, CalculusFieldElement)46100%n/a010301
getMeanAnomalyDot()45100%4100%030801
trueToEllipticEccentric(CalculusFieldElement, CalculusFieldElement)44100%n/a010301
getEccentricAnomalyDot()41100%4100%030801
getEquinoctialExDot()38100%2100%020601
getEquinoctialEyDot()38100%2100%020601
checkParameterRangeInclusive(String, double, double, double)35100%1375%130401
trueToHyperbolicEccentric(CalculusFieldElement, CalculusFieldElement)32100%n/a010301
getHx()31100%2100%020301
getHy()31100%2100%020301
hyperbolicEccentricToTrue(CalculusFieldElement, CalculusFieldElement)29100%n/a010301
getMeanAnomaly()24100%2100%020301
FieldKeplerianOrbit(CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, PositionAngle, Frame, FieldAbsoluteDate, CalculusFieldElement)19100%n/a010201
getEccentricAnomaly()18100%2100%020101
getLvDot()16100%2100%020201
getLEDot()16100%2100%020201
getLMDot()16100%2100%020201
getAnomaly(PositionAngle)15100%4100%030301
getAnomalyDot(PositionAngle)15100%4100%030301
getEquinoctialEx()12100%n/a010101
getEquinoctialEy()12100%n/a010101
computeJacobianMeanWrtCartesian()12100%2100%020301
computeJacobianEccentricWrtCartesian()12100%2100%020301
computeJacobianTrueWrtCartesian()12100%2100%020301
FieldKeplerianOrbit(FieldOrbit)11100%n/a010201
getLv()11100%n/a010101
getLE()11100%n/a010101
getLM()11100%n/a010101
shiftedBy(double)11100%n/a010101
static {...}11100%n/a010601
FieldKeplerianOrbit(FieldPVCoordinates, Frame, FieldAbsoluteDate, CalculusFieldElement)10100%n/a010201
FieldKeplerianOrbit(TimeStampedFieldPVCoordinates, Frame, CalculusFieldElement)9100%n/a010201
hyperbolicEccentricToMean(CalculusFieldElement, CalculusFieldElement)9100%n/a010101
ellipticEccentricToMean(CalculusFieldElement, CalculusFieldElement)8100%n/a010101
hasDerivatives()7100%2100%020101
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