FieldCircularOrbit

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total45 of 4,86099%9 of 12092%91359621066
addKeplerContribution(PositionAngleType, CalculusFieldElement, CalculusFieldElement[])13996%1375%1411501
initializeCachedAlpha(CalculusFieldElement, CalculusFieldElement, PositionAngleType)8394%11191%1811601
getAlphaVDot()8094%1583%1511501
getAlphaEDot()8094%1583%1511501
getAlphaMDot()8094%1583%1511501
initializeCachedAlpha(CalculusFieldElement, PositionAngleType)6392%11191%1811301
getAlphaV()2583%1375%141501
getAlphaE()2583%1375%141501
getAlphaM()2583%1375%141501
computeJacobianMeanWrtCartesian()1,144100%n/a01011101
FieldCircularOrbit(TimeStampedFieldPVCoordinates, Frame, CalculusFieldElement)590100%4100%0306501
computePVWithoutA()329100%2100%0203901
FieldCircularOrbit(FieldOrbit)252100%6100%0403901
initPosition()223100%n/a0102801
nonKeplerianAcceleration()218100%n/a0102201
computeJacobianTrueWrtCartesian()201100%2100%0202401
FieldCircularOrbit(Field, CircularOrbit)147100%2100%0202301
shiftedBy(CalculusFieldElement)116100%2100%0201801
FieldCircularOrbit(CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, PositionAngleType, PositionAngleType, Frame, FieldAbsoluteDate, CalculusFieldElement)96100%4100%0302401
computeJacobianEccentricWrtCartesian()88100%2100%0201301
toOrbit()85100%2100%0201201
getHxDot()68100%4100%030801
getHyDot()68100%4100%030801
initPVCoordinates()51100%2100%020801
toString()50100%n/a010701
getEquinoctialExDot()42100%2100%020501
getEquinoctialEyDot()42100%2100%020501
getHx()33100%2100%020301
getHy()33100%2100%020301
getEDot()24100%2100%020301
removeRates()24100%n/a010301
getEquinoctialEx()21100%n/a010201
getEquinoctialEy()21100%n/a010201
FieldCircularOrbit(CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, PositionAngleType, PositionAngleType, Frame, FieldAbsoluteDate, CalculusFieldElement)20100%n/a010201
FieldCircularOrbit(CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, PositionAngleType, Frame, FieldAbsoluteDate, CalculusFieldElement)20100%n/a010201
getE()17100%n/a010101
getAlpha(PositionAngleType)15100%4100%030301
getAlphaDot(PositionAngleType)15100%4100%030301
FieldCircularOrbit(CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, PositionAngleType, Frame, FieldAbsoluteDate, CalculusFieldElement)14100%n/a010201
getLvDot()12100%2100%020101
getLEDot()12100%2100%020101
getLMDot()12100%2100%020101
FieldCircularOrbit(FieldPVCoordinates, Frame, FieldAbsoluteDate, CalculusFieldElement)10100%n/a010201
FieldCircularOrbit(Field, Orbit)100%n/a010201
shiftedBy(double)100%n/a010101
getLv()100%n/a010101
getLE()100%n/a010101
getLM()100%n/a010101
hasDerivatives()100%2100%020101
eccentricToTrue(CalculusFieldElement, CalculusFieldElement, CalculusFieldElement)100%n/a010101
trueToEccentric(CalculusFieldElement, CalculusFieldElement, CalculusFieldElement)100%n/a010101
meanToEccentric(CalculusFieldElement, CalculusFieldElement, CalculusFieldElement)100%n/a010101
eccentricToMean(CalculusFieldElement, CalculusFieldElement, CalculusFieldElement)100%n/a010101
getA()100%n/a010101
getADot()100%n/a010101
getCircularEx()100%n/a010101
getCircularExDot()100%n/a010101
getCircularEy()100%n/a010101
getCircularEyDot()100%n/a010101
getI()100%n/a010101
getIDot()100%n/a010101
getRightAscensionOfAscendingNode()100%n/a010101
getRightAscensionOfAscendingNodeDot()100%n/a010101
getCachedPositionAngleType()100%n/a010101
hasRates()100%n/a010101
getType()100%n/a010101