FieldKeplerianOrbit

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total43 of 5,32999%5 of 14696%61456691169
normalizeAngle(RealFieldElement, RealFieldElement)160%n/a111111
meanToHyperbolicEccentric(RealFieldElement, RealFieldElement)1213992%21487%2922301
FieldKeplerianOrbit(RealFieldElement, RealFieldElement, RealFieldElement, RealFieldElement, RealFieldElement, RealFieldElement, RealFieldElement, RealFieldElement, RealFieldElement, RealFieldElement, RealFieldElement, RealFieldElement, PositionAngle, Frame, FieldAbsoluteDate, RealFieldElement)1029796%22291%21525601
addKeplerContribution(PositionAngle, RealFieldElement, RealFieldElement[])11995%1375%1411501
computeJacobianMeanWrtCartesianElliptical()774100%n/a0108401
computeJacobianMeanWrtCartesianHyperbolic()747100%n/a0108801
FieldKeplerianOrbit(TimeStampedFieldPVCoordinates, Frame, RealFieldElement, boolean)530100%8100%0506401
interpolate(FieldAbsoluteDate, Stream)299100%12100%0704701
computePVWithoutA()292100%4100%0303801
meanToEllipticEccentric(RealFieldElement, RealFieldElement)262100%12100%0702801
nonKeplerianAcceleration()203100%n/a0102201
shiftedBy(RealFieldElement)114100%2100%0201601
computeJacobianTrueWrtCartesianElliptical()92100%2100%0201501
computeJacobianTrueWrtCartesianHyperbolic()88100%2100%0201501
toOrbit()83100%2100%020901
getHxDot()72100%4100%030801
getHyDot()72100%4100%030801
getMeanAnomalyDot()71100%4100%030901
getEquinoctialExDot()71100%2100%020701
getEquinoctialEyDot()71100%2100%020701
getEccentricAnomalyDot()67100%4100%030901
eMeSinE(RealFieldElement, RealFieldElement)63100%2100%0201001
computeJacobianEccentricWrtCartesianElliptical()60100%2100%0201001
computeJacobianEccentricWrtCartesianHyperbolic()58100%2100%0201001
toString()51100%n/a010801
initPVCoordinates()49100%2100%020701
ellipticEccentricToTrue(RealFieldElement, RealFieldElement)41100%n/a010201
trueToEllipticEccentric(RealFieldElement, RealFieldElement)39100%n/a010201
hyperbolicEccentricToTrue(RealFieldElement, RealFieldElement)29100%n/a010301
getHx()28100%2100%020301
getHy()28100%2100%020301
trueToHyperbolicEccentric(RealFieldElement, RealFieldElement)27100%n/a010201
getMeanAnomaly()24100%2100%020301
FieldKeplerianOrbit(RealFieldElement, RealFieldElement, RealFieldElement, RealFieldElement, RealFieldElement, RealFieldElement, PositionAngle, Frame, FieldAbsoluteDate, RealFieldElement)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
static {...}15100%n/a010701
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
FieldKeplerianOrbit(FieldPVCoordinates, Frame, FieldAbsoluteDate, RealFieldElement)10100%n/a010201
FieldKeplerianOrbit(TimeStampedFieldPVCoordinates, Frame, RealFieldElement)9100%n/a010201
hyperbolicEccentricToMean(RealFieldElement, RealFieldElement)9100%n/a010101
ellipticEccentricToMean(RealFieldElement, RealFieldElement)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