CircularOrbit

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total99 of 2,46396%8 of 3476%95410311134
toString()440%n/a111111
CircularOrbit(double, double, double, double, double, double, PositionAngle, TimeStampedPVCoordinates, Frame, double)324357%4233%4561801
CircularOrbit(TimeStampedPVCoordinates, Frame, double)1322094%1150%1213501
addKeplerContribution(PositionAngle, double, double[])11296%1375%1411401
CircularOrbit(double, double, double, double, double, double, PositionAngle, Frame, AbsoluteDate, double)7093%1583%1511801
computeJacobianMeanWrtCartesian()877100%n/a0107801
initPVCoordinates()255100%n/a0103301
computeJacobianTrueWrtCartesian()156100%2100%0202301
interpolate(AbsoluteDate, Collection)137100%4100%0302001
meanToEccentric(double)81100%1375%1301701
computeJacobianEccentricWrtCartesian()67100%2100%0201101
CircularOrbit(Orbit)66100%n/a0101301
getAlphaE()53100%n/a010401
eccentricToTrue(double)50100%n/a010401
shiftedBy(double)30100%n/a010101
getAlphaM()17100%n/a010201
getAlpha(PositionAngle)15100%4100%030101
getEquinoctialEx()14100%n/a010101
getEquinoctialEy()14100%n/a010101
getE()13100%n/a010101
CircularOrbit(PVCoordinates, Frame, AbsoluteDate, double)10100%n/a010201
getHx()10100%n/a010101
getHy()10100%n/a010101
getLv()100%n/a010101
getLE()100%n/a010101
getLM()100%n/a010101
writeReplace()100%n/a010101
getA()100%n/a010101
getCircularEx()100%n/a010101
getCircularEy()100%n/a010101
getAlphaV()100%n/a010101
getI()100%n/a010101
getRightAscensionOfAscendingNode()100%n/a010101
getType()100%n/a010101