FieldCartesianOrbit

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total19 of 2,07999%7 of 7090%7803297045
meanToHyperbolicEccentric(RealFieldElement, RealFieldElement)1214692%21487%2922301
meanToEccentric(RealFieldElement, RealFieldElement, RealFieldElement)79092%1375%1311601
shiftPVElliptic(RealFieldElement)414100%2100%0204201
shiftPVHyperbolic(RealFieldElement)329100%2100%0204101
addKeplerContribution(PositionAngle, double, RealFieldElement[])96100%n/a0101201
getE()75100%2100%0201001
getHxDot()70100%1583%1401101
getHyDot()69100%1583%1401101
getEDot()68100%2100%0201201
FieldCartesianOrbit(FieldOrbit)67100%6100%0401301
getPositionDS()60100%n/a010601
getVelocityDS()60100%n/a010601
FieldCartesianOrbit(TimeStampedFieldPVCoordinates, Frame, double)49100%2100%020901
getHx()49100%1375%130701
getHy()47100%1375%130701
initEquinoctial()41100%4100%030701
toOrbit()38100%2100%020601
getADot()36100%2100%020601
create6x6Identity()29100%2100%020501
getA()27100%n/a010301
shiftedBy(RealFieldElement)27100%2100%020201
getIDot()25100%2100%020601
interpolate(FieldAbsoluteDate, Stream)17100%n/a010401
getI()14100%n/a010101
shiftedBy(double)11100%n/a010101
toString()11100%n/a010101
FieldCartesianOrbit(FieldPVCoordinates, Frame, FieldAbsoluteDate, double)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
static {...}5100%n/a010101
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