FieldKeplerianOrbit

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total45 of 4,92099%11 of 17493%111659667070
FieldKeplerianOrbit(TimeStampedFieldPVCoordinates, Frame, CalculusFieldElement, boolean)950898%2880%2616801
initializeCachedAnomaly(CalculusFieldElement, CalculusFieldElement, PositionAngleType)12095%22291%21522701
getTrueAnomalyDot()8494%1990%1711701
getEccentricAnomalyDot()8494%1990%1711701
getMeanAnomalyDot()8494%1990%1711701
getTrueAnomaly()4590%1787%161701
getEccentricAnomaly()4590%1787%161701
getMeanAnomaly()4590%1787%161701
computeJacobianMeanWrtCartesianElliptical()792100%n/a0108601
computeJacobianMeanWrtCartesianHyperbolic()750100%n/a0108901
computePVWithoutA()222100%4100%0302801
nonKeplerianAcceleration()218100%n/a0102201
FieldKeplerianOrbit(CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, PositionAngleType, PositionAngleType, Frame, FieldAbsoluteDate, CalculusFieldElement)171100%8100%0503101
FieldKeplerianOrbit(Field, KeplerianOrbit)138100%12100%0701201
initPosition()120100%2100%0201401
shiftedBy(CalculusFieldElement)116100%2100%0201701
referenceAxes()113100%n/a0101701
computeKeplerianAnomalyDot(PositionAngleType, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, PositionAngleType)96100%4100%0301201
toOrbit()89100%2100%0201101
computeJacobianTrueWrtCartesianElliptical()88100%2100%0201301
computeJacobianTrueWrtCartesianHyperbolic()87100%2100%0201501
computeJacobianEccentricWrtCartesianHyperbolic()60100%2100%0201001
computeJacobianEccentricWrtCartesianElliptical()59100%2100%020801
getHxDot()51100%4100%030701
getHyDot()51100%4100%030701
toString()51100%n/a010801
initPVCoordinates()50100%2100%020801
getEquinoctialExDot()38100%2100%020601
getEquinoctialEyDot()38100%2100%020601
checkParameterRangeInclusive(String, double, double, double)35100%1375%130401
getHx()33100%2100%020301
getHy()33100%2100%020301
removeRates()24100%n/a010201
FieldKeplerianOrbit(CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, PositionAngleType, PositionAngleType, Frame, FieldAbsoluteDate, CalculusFieldElement)20100%n/a010201
FieldKeplerianOrbit(CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, PositionAngleType, Frame, FieldAbsoluteDate, CalculusFieldElement)20100%n/a010201
addKeplerContribution(PositionAngleType, CalculusFieldElement, CalculusFieldElement[])20100%n/a010201
getLvDot()16100%2100%020301
getLEDot()16100%2100%020301
getLMDot()16100%2100%020301
getAnomaly(PositionAngleType)15100%4100%030301
getAnomalyDot(PositionAngleType)15100%4100%030301
FieldKeplerianOrbit(CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, PositionAngleType, Frame, FieldAbsoluteDate, CalculusFieldElement)14100%n/a010201
getEquinoctialEx()13100%n/a010101
getEquinoctialEy()13100%n/a010101
FieldKeplerianOrbit(FieldOrbit)11100%n/a010201
getLv()11100%n/a010101
getLE()11100%n/a010101
getLM()11100%n/a010101
FieldKeplerianOrbit(FieldPVCoordinates, Frame, FieldAbsoluteDate, CalculusFieldElement)10100%n/a010201
FieldKeplerianOrbit(TimeStampedFieldPVCoordinates, Frame, CalculusFieldElement)9100%n/a010201
computeJacobianMeanWrtCartesian()9100%2100%020301
computeJacobianEccentricWrtCartesian()9100%2100%020301
computeJacobianTrueWrtCartesian()9100%2100%020301
FieldKeplerianOrbit(Field, Orbit)8100%n/a010201
initializeCachedAnomaly(CalculusFieldElement, PositionAngleType)8100%n/a010101
shiftedBy(double)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
getCachedPositionAngleType()100%n/a010101
hasRates()100%n/a010101
getType()100%n/a010101