FieldEquinoctialOrbit

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total28 of 3,71399%5 of 5691%5815449050
FieldEquinoctialOrbit(TimeStampedFieldPVCoordinates, Frame, CalculusFieldElement)1349097%1375%1325501
FieldEquinoctialOrbit(CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, PositionAngleType, Frame, FieldAbsoluteDate, CalculusFieldElement)1015293%21083%2924001
addKeplerContribution(PositionAngleType, CalculusFieldElement, CalculusFieldElement[])15096%1375%1411501
computeJacobianMeanWrtCartesian()690100%n/a0105701
computePVWithoutA()337100%2100%0203501
initPosition()230100%n/a0102401
nonKeplerianAcceleration()218100%n/a0102201
computeJacobianTrueWrtCartesian()198100%2100%0202301
FieldEquinoctialOrbit(Field, EquinoctialOrbit)136100%2100%0202101
shiftedBy(CalculusFieldElement)115100%2100%0201801
meanToEccentric(CalculusFieldElement, CalculusFieldElement, CalculusFieldElement)104100%1375%1301501
toOrbit()83100%2100%0201101
computeJacobianEccentricWrtCartesian()82100%2100%0201101
eccentricToTrue(CalculusFieldElement, CalculusFieldElement, CalculusFieldElement)70100%n/a010701
trueToEccentric(CalculusFieldElement, CalculusFieldElement, CalculusFieldElement)70100%n/a010701
FieldEquinoctialOrbit(FieldOrbit)57100%n/a0101401
getIDot()51100%2100%020501
initPVCoordinates()51100%2100%020801
toString()48100%n/a010601
getLMDot()43100%2100%020701
getLEDot()39100%2100%020701
getEDot()38100%2100%020301
removeRates()27100%n/a010301
getI()22100%n/a010101
eccentricToMean(CalculusFieldElement, CalculusFieldElement, CalculusFieldElement)21100%n/a010201
FieldEquinoctialOrbit(CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, PositionAngleType, Frame, FieldAbsoluteDate, CalculusFieldElement)19100%n/a010201
getE()17100%n/a010101
getL(PositionAngleType)15100%4100%030301
getLDot(PositionAngleType)15100%4100%030301
getLM()13100%n/a010101
FieldEquinoctialOrbit(FieldPVCoordinates, Frame, FieldAbsoluteDate, CalculusFieldElement)10100%n/a010201
FieldEquinoctialOrbit(Field, Orbit)8100%n/a010201
getLE()8100%n/a010101
shiftedBy(double)8100%n/a010101
hasDerivatives()7100%2100%020101
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
getLv()100%n/a010101
getLvDot()100%n/a010101
hasRates()100%n/a010101
getType()100%n/a010101
getCachedPositionAngleType()100%n/a010101