FieldCartesianOrbit

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total3 of 1,66399%3 of 4893%3661269042
FieldCartesianOrbit(Field, CartesianOrbit)33692%1150%121701
shiftPVHyperbolic(CalculusFieldElement)325100%2100%0204201
shiftPVElliptic(CalculusFieldElement)319100%2100%0204301
addKeplerContribution(PositionAngleType, CalculusFieldElement, CalculusFieldElement[])96100%n/a0101201
getPVDerivatives()80100%n/a0101101
getE()74100%2100%0201101
getHxDot()68100%1583%1401201
getHyDot()67100%1583%1401201
getEDot()62100%2100%0201101
getHx()49100%4100%030701
toString()49100%n/a0101101
getHy()47100%4100%030701
initEquinoctial()42100%4100%030701
toOrbit()40100%2100%020601
getADot()34100%2100%020701
FieldCartesianOrbit(FieldOrbit)33100%4100%030801
create6x6Identity()29100%2100%020501
getA()28100%n/a010401
shiftedBy(CalculusFieldElement)24100%2100%020201
getIDot()23100%2100%020701
FieldCartesianOrbit(TimeStampedFieldPVCoordinates, Frame, CalculusFieldElement)14100%n/a010401
getI()14100%n/a010101
FieldCartesianOrbit(FieldPVCoordinates, Frame, FieldAbsoluteDate, CalculusFieldElement)10100%n/a010201
FieldCartesianOrbit(Field, Orbit)8100%n/a010201
shiftedBy(double)8100%n/a010101
getEquinoctialEx()6100%n/a010201
getEquinoctialExDot()6100%n/a010201
getEquinoctialEy()6100%n/a010201
getEquinoctialEyDot()6100%n/a010201
getLv()6100%n/a010201
getLvDot()6100%n/a010201
getLE()6100%n/a010201
getLEDot()6100%n/a010201
getLM()6100%n/a010201
getLMDot()6100%n/a010201
initPosition()4100%n/a010101
hasDerivatives()3100%n/a010101
initPVCoordinates()3100%n/a010101
computeJacobianMeanWrtCartesian()3100%n/a010101
computeJacobianEccentricWrtCartesian()3100%n/a010101
computeJacobianTrueWrtCartesian()3100%n/a010101
getType()100%n/a010101