FieldKeplerianOrbit

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total6 of 4,17699%5 of 12696%51412563074
initializeCachedAnomaly(CalculusFieldElement, CalculusFieldElement, PositionAngleType)12095%22291%21522701
computeJacobianMeanWrtCartesianElliptical()792100%n/a0108601
computeJacobianMeanWrtCartesianHyperbolic()750100%n/a0108901
FieldKeplerianOrbit(TimeStampedFieldPVCoordinates, Frame, CalculusFieldElement, boolean)366100%4100%0304501
FieldKeplerianOrbit(FieldKeplerianParameters, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, PositionAngleType, Frame, FieldAbsoluteDate, CalculusFieldElement)174100%6100%0402801
initPosition()125100%2100%0201401
computeKeplerianAnomalyDot(PositionAngleType, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, PositionAngleType)96100%4100%0301201
computeJacobianTrueWrtCartesianElliptical()88100%2100%0201301
computeJacobianTrueWrtCartesianHyperbolic()87100%2100%0201501
getTrueAnomalyDot()83100%7100%0501401
getEccentricAnomalyDot()83100%7100%0501401
getMeanAnomalyDot()83100%7100%0501401
applyNonKeplerianAcceleration(FieldVector3D, CalculusFieldElement)74100%n/a0101201
FieldKeplerianOrbit(Field, KeplerianOrbit)70100%n/a0101001
computeJacobianEccentricWrtCartesianHyperbolic()60100%2100%0201001
computeJacobianEccentricWrtCartesianElliptical()59100%2100%020801
toOrbit()57100%n/a010601
hasNonKeplerianAcceleration()56100%21083%270201
getHxDot()52100%4100%030701
getHyDot()52100%4100%030701
initPVCoordinates()50100%2100%020801
inFrame(Frame)42100%4100%030801
FieldKeplerianOrbit(FieldKeplerianParameters, Frame, FieldAbsoluteDate, CalculusFieldElement)41100%n/a010501
shiftWithKeplerianMotion(TimeOffset)41100%n/a010401
shiftWithKeplerianMotion(CalculusFieldElement)40100%n/a010401
getEquinoctialExDot()39100%2100%020601
getEquinoctialEyDot()39100%2100%020601
withCachedPositionAngleType(PositionAngleType)37100%n/a010201
checkParameterRangeInclusive(String, double, double, double)35100%1375%130401
getHx()33100%2100%020301
getHy()33100%2100%020301
shiftedBy(TimeOffset)29100%4100%030601
toString()24100%n/a010701
FieldKeplerianOrbit(CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, PositionAngleType, Frame, FieldAbsoluteDate, CalculusFieldElement)23100%n/a010201
addKeplerContribution(PositionAngleType, CalculusFieldElement, CalculusFieldElement[])20100%n/a010201
getKeplerianParameters()18100%n/a010101
shiftedBy(CalculusFieldElement)18100%4100%030401
getAnomalyDot(PositionAngleType)17100%3100%030401
computePVWithoutA()17100%2100%020501
FieldKeplerianOrbit(CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, PositionAngleType, Frame, FieldAbsoluteDate, CalculusFieldElement)16100%n/a010201
getEquinoctialEx()13100%n/a010101
getEquinoctialEy()13100%n/a010101
withKeplerianRates()12100%n/a010101
getLv()11100%n/a010101
getLvDot()11100%n/a010101
getLE()11100%n/a010101
getLEDot()11100%n/a010101
getLM()11100%n/a010101
getLMDot()11100%n/a010101
FieldKeplerianOrbit(FieldPVCoordinates, Frame, FieldAbsoluteDate, CalculusFieldElement)10100%n/a010201
FieldKeplerianOrbit(TimeStampedFieldPVCoordinates, Frame, CalculusFieldElement)9100%n/a010201
FieldKeplerianOrbit(FieldOrbit)9100%n/a010201
computeJacobianMeanWrtCartesian()9100%2100%020301
computeJacobianEccentricWrtCartesian()9100%2100%020301
computeJacobianTrueWrtCartesian()9100%2100%020301
FieldKeplerianOrbit(Field, Orbit)8100%n/a010201
shiftedBy(double)8100%n/a010101
getAnomaly(PositionAngleType)100%n/a010101
getTrueAnomaly()100%n/a010101
getEccentricAnomaly()100%n/a010101
getMeanAnomaly()100%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
getCachedPositionAngleType()100%n/a010101
hasNonKeplerianRates()100%n/a010101
getType()100%n/a010101