FieldKeplerianOrbit

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total31 of 5,76199%6 of 14895%61485734071
meanToHyperbolicEccentric(RealFieldElement, RealFieldElement)1214892%21487%2922301
FieldKeplerianOrbit(RealFieldElement, RealFieldElement, RealFieldElement, RealFieldElement, RealFieldElement, RealFieldElement, RealFieldElement, RealFieldElement, RealFieldElement, RealFieldElement, RealFieldElement, RealFieldElement, PositionAngle, Frame, FieldAbsoluteDate, double)1030196%22291%21525601
addKeplerContribution(PositionAngle, double, RealFieldElement[])12596%1375%1411501
ellipticKeplerianToPosition(RealFieldElement, RealFieldElement, RealFieldElement, RealFieldElement, RealFieldElement, RealFieldElement, double)14897%1150%1202001
computeJacobianMeanWrtCartesianElliptical()788100%n/a0108401
computeJacobianMeanWrtCartesianHyperbolic()751100%n/a0108801
FieldKeplerianOrbit(TimeStampedFieldPVCoordinates, Frame, double, boolean)551100%8100%0506401
computePVWithoutA()307100%4100%0303801
interpolate(FieldAbsoluteDate, Stream)300100%12100%0704701
meanToEllipticEccentric(RealFieldElement, RealFieldElement)285100%12100%0702801
nonKeplerianAcceleration()218100%n/a0102201
hyperbolicKeplerianToPosition(RealFieldElement, RealFieldElement, RealFieldElement, RealFieldElement, RealFieldElement, RealFieldElement, double)140100%n/a0101901
shiftedBy(RealFieldElement)114100%2100%0201601
computeJacobianTrueWrtCartesianElliptical()93100%2100%0201501
computeJacobianTrueWrtCartesianHyperbolic()89100%2100%0201501
toOrbit()81100%2100%020901
getMeanAnomalyDot()73100%4100%030901
getHxDot()72100%4100%030801
getHyDot()72100%4100%030801
getEquinoctialExDot()71100%2100%020701
getEquinoctialEyDot()71100%2100%020701
getEccentricAnomalyDot()67100%4100%030901
eMeSinE(RealFieldElement, RealFieldElement)63100%2100%0201001
computeJacobianEccentricWrtCartesianElliptical()62100%2100%0201001
computeJacobianEccentricWrtCartesianHyperbolic()60100%2100%0201001
toString()51100%n/a010801
initPVCoordinates()50100%2100%020801
ellipticEccentricToTrue(RealFieldElement, RealFieldElement)46100%n/a010201
trueToEllipticEccentric(RealFieldElement, RealFieldElement)44100%n/a010201
hyperbolicEccentricToTrue(RealFieldElement, RealFieldElement)30100%n/a010301
trueToHyperbolicEccentric(RealFieldElement, RealFieldElement)30100%n/a010201
getHx()29100%2100%020301
getHy()29100%2100%020301
getMeanAnomaly()24100%2100%020301
FieldKeplerianOrbit(RealFieldElement, RealFieldElement, RealFieldElement, RealFieldElement, RealFieldElement, RealFieldElement, PositionAngle, Frame, FieldAbsoluteDate, double)19100%n/a010201
getEccentricAnomaly()18100%2100%020101
getLvDot()16100%2100%020301
getLEDot()16100%2100%020301
getLMDot()16100%2100%020301
normalizeAngle(RealFieldElement, RealFieldElement)16100%n/a010101
getAnomaly(PositionAngle)15100%4100%030301
getAnomalyDot(PositionAngle)15100%4100%030301
static {...}15100%n/a010701
getEquinoctialEx()13100%n/a010101
getEquinoctialEy()13100%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, double)10100%n/a010201
hyperbolicEccentricToMean(RealFieldElement, RealFieldElement)10100%n/a010101
ellipticEccentricToMean(RealFieldElement, RealFieldElement)10100%n/a010101
FieldKeplerianOrbit(TimeStampedFieldPVCoordinates, Frame, double)9100%n/a010201
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