CircularOrbit

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total28 of 3,68499%5 of 6892%5935493056
CircularOrbit(TimeStampedPVCoordinates, Frame, double)1347497%1375%1326301
CircularOrbit(double, double, double, double, double, double, double, double, double, double, double, double, PositionAngle, Frame, AbsoluteDate, double)1015093%21083%2924101
addKeplerContribution(PositionAngle, double, double[])11295%1375%1411501
computeJacobianMeanWrtCartesian()883100%n/a0108001
interpolate(AbsoluteDate, Stream)286100%12100%0704201
computePVWithoutA()245100%2100%0203501
CircularOrbit(Orbit)211100%6100%0403701
nonKeplerianAcceleration()180100%n/a010701
computeJacobianTrueWrtCartesian()159100%2100%0202401
shiftedBy(double)102100%2100%0201501
meanToEccentric(double, double, double)75100%1375%1301501
computeJacobianEccentricWrtCartesian()70100%2100%0201201
CircularOrbit(double, double, double, double, double, double, double, double, double, double, double, double, TimeStampedPVCoordinates, Frame, double)48100%n/a0101601
initPVCoordinates()45100%2100%020601
toString()44100%n/a010701
eccentricToTrue(double, double, double)43100%n/a010401
trueToEccentric(double, double, double)43100%n/a010401
getHxDot()42100%2100%020501
getHyDot()42100%2100%020501
getAlphaMDot()37100%n/a010501
getAlphaEDot()34100%n/a010501
getEquinoctialExDot()28100%n/a010201
getEquinoctialEyDot()28100%n/a010201
getHx()20100%2100%020301
getHy()20100%2100%020301
CircularOrbit(double, double, double, double, double, double, PositionAngle, Frame, AbsoluteDate, double)19100%n/a010201
getEquinoctialEx()16100%n/a010201
getEquinoctialEy()16100%n/a010201
getAlpha(PositionAngle)15100%4100%030301
getAlphaDot(PositionAngle)15100%4100%030301
eccentricToMean(double, double, double)15100%n/a010201
getEDot()15100%n/a010101
getAlphaM()13100%n/a010101
getE()13100%n/a010101
CircularOrbit(PVCoordinates, Frame, AbsoluteDate, double)10100%n/a010201
getAlphaE()8100%n/a010101
getLv()100%n/a010101
getLvDot()100%n/a010101
getLE()100%n/a010101
getLEDot()100%n/a010101
getLM()100%n/a010101
getLMDot()100%n/a010101
writeReplace()100%n/a010101
getA()100%n/a010101
getADot()100%n/a010101
getCircularEx()100%n/a010101
getCircularExDot()100%n/a010101
getCircularEy()100%n/a010101
getCircularEyDot()100%n/a010101
getAlphaV()100%n/a010101
getAlphaVDot()100%n/a010101
getI()100%n/a010101
getIDot()100%n/a010101
getRightAscensionOfAscendingNode()100%n/a010101
getRightAscensionOfAscendingNodeDot()100%n/a010101
getType()100%n/a010101