FieldCartesianOrbit

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total7 of 1,82999%3 of 5094%3671282042
meanToEccentric(CalculusFieldElement, CalculusFieldElement, CalculusFieldElement)78892%1375%1311501
shiftPVElliptic(CalculusFieldElement)402100%2100%0204401
shiftPVHyperbolic(CalculusFieldElement)313100%2100%0204101
addKeplerContribution(PositionAngle, CalculusFieldElement, CalculusFieldElement[])92100%n/a0101201
getPVDerivatives()80100%n/a0101101
getE()73100%2100%0201001
getHxDot()68100%1583%1401201
getHyDot()67100%1583%1401201
getEDot()62100%2100%0201101
FieldCartesianOrbit(FieldOrbit)50100%4100%0301101
toString()49100%n/a0101101
getHx()48100%4100%030701
getHy()46100%4100%030701
initEquinoctial()41100%4100%030701
toOrbit()40100%2100%020601
getADot()34100%2100%020701
FieldCartesianOrbit(TimeStampedFieldPVCoordinates, Frame, CalculusFieldElement)32100%n/a010701
create6x6Identity()29100%2100%020501
shiftedBy(CalculusFieldElement)27100%2100%020201
getA()26100%n/a010301
getIDot()23100%2100%020701
interpolate(FieldAbsoluteDate, Stream)17100%n/a010401
getI()14100%n/a010101
shiftedBy(double)11100%n/a010101
FieldCartesianOrbit(FieldPVCoordinates, Frame, FieldAbsoluteDate, CalculusFieldElement)10100%n/a010201
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
hasDerivatives()100%n/a010101
initPVCoordinates()100%n/a010101
computeJacobianMeanWrtCartesian()100%n/a010101
computeJacobianEccentricWrtCartesian()100%n/a010101
computeJacobianTrueWrtCartesian()100%n/a010101
lambda$interpolate$0(FieldOrbit)100%n/a010101
getType()100%n/a010101