FieldEquinoctialOrbit

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total45 of 3,77998%9 of 9490%91109484054
addKeplerContribution(PositionAngleType, CalculusFieldElement, CalculusFieldElement[])13296%1375%1411501
initializeCachedL(CalculusFieldElement, CalculusFieldElement, PositionAngleType)8394%11191%1811601
getLvDot()8094%1583%1511501
getLEDot()8094%1583%1511501
getLMDot()8094%1583%1511501
initializeCachedL(CalculusFieldElement, PositionAngleType)6392%11191%1811301
getLv()2583%1375%141501
getLE()2583%1375%141501
getLM()2583%1375%141501
computeJacobianMeanWrtCartesian()680100%n/a0105701
FieldEquinoctialOrbit(TimeStampedFieldPVCoordinates, Frame, CalculusFieldElement)499100%4100%0305601
computePVWithoutA()329100%2100%0203501
initPosition()222100%n/a0102401
nonKeplerianAcceleration()218100%n/a0102201
computeJacobianTrueWrtCartesian()194100%2100%0202301
FieldEquinoctialOrbit(Field, EquinoctialOrbit)144100%2100%0202201
shiftedBy(CalculusFieldElement)116100%2100%0201801
FieldEquinoctialOrbit(CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, PositionAngleType, PositionAngleType, Frame, FieldAbsoluteDate, CalculusFieldElement)96100%4100%0302401
toOrbit()85100%2100%0201201
computeJacobianEccentricWrtCartesian()82100%2100%0201101
FieldEquinoctialOrbit(FieldOrbit)60100%n/a0101501
initPVCoordinates()51100%2100%020801
toString()48100%n/a010601
getIDot()47100%2100%020501
getEDot()34100%2100%020301
removeRates()24100%n/a010201
FieldEquinoctialOrbit(CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, PositionAngleType, PositionAngleType, Frame, FieldAbsoluteDate, CalculusFieldElement)20100%n/a010201
FieldEquinoctialOrbit(CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, PositionAngleType, Frame, FieldAbsoluteDate, CalculusFieldElement)20100%n/a010201
FieldEquinoctialOrbit(CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, PositionAngleType, Frame, FieldAbsoluteDate, CalculusFieldElement)20100%n/a010201
getI()18100%n/a010101
getL(PositionAngleType)15100%4100%030301
getLDot(PositionAngleType)15100%4100%030301
getE()13100%n/a010101
FieldEquinoctialOrbit(FieldPVCoordinates, Frame, FieldAbsoluteDate, CalculusFieldElement)10100%n/a010201
FieldEquinoctialOrbit(Field, Orbit)8100%n/a010201
shiftedBy(double)8100%n/a010101
hasDerivatives()7100%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
getEquinoctialEx()100%n/a010101
getEquinoctialExDot()100%n/a010101
getEquinoctialEy()100%n/a010101
getEquinoctialEyDot()100%n/a010101
getHx()100%n/a010101
getHxDot()100%n/a010101
getHy()100%n/a010101
getHyDot()100%n/a010101
getCachedPositionAngleType()100%n/a010101
hasRates()100%n/a010101
getType()100%n/a010101