EquinoctialOrbit

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total28 of 2,86699%5 of 5490%5735385043
EquinoctialOrbit(TimeStampedPVCoordinates, Frame, double)1340496%1375%1325401
EquinoctialOrbit(double, double, double, double, double, double, double, double, double, double, double, double, PositionAngle, Frame, AbsoluteDate, double)1014793%21083%2924001
addKeplerContribution(PositionAngle, double, double[])511295%1375%1411401
computeJacobianMeanWrtCartesian()532100%n/a0105201
interpolate(AbsoluteDate, Stream)276100%12100%0704001
computePVWithoutA()250100%2100%0203001
nonKeplerianAcceleration()180100%n/a010701
computeJacobianTrueWrtCartesian()156100%2100%0202301
shiftedBy(double)102100%2100%0201501
meanToEccentric(double, double, double)77100%1375%1301701
computeJacobianEccentricWrtCartesian()67100%2100%0201101
EquinoctialOrbit(Orbit)60100%n/a0101501
eccentricToTrue(double, double, double)46100%n/a010601
trueToEccentric(double, double, double)46100%n/a010601
initPVCoordinates()45100%2100%020601
toString()42100%n/a010601
getLMDot()37100%n/a010501
getIDot()35100%n/a010301
getLEDot()34100%n/a010501
getEDot()25100%n/a010101
EquinoctialOrbit(double, double, double, double, double, double, PositionAngle, Frame, AbsoluteDate, double)19100%n/a010201
getI()16100%n/a010101
getL(PositionAngle)15100%4100%030301
getLDot(PositionAngle)15100%4100%030301
getLM()13100%n/a010101
getE()13100%n/a010101
eccentricToMean(double, double, double)12100%n/a010101
EquinoctialOrbit(PVCoordinates, Frame, AbsoluteDate, double)10100%n/a010201
getLE()8100%n/a010101
writeReplace()6100%n/a010101
getA()100%n/a010101
getADot()100%n/a010101
getEquinoctialEx()100%n/a010101
getEquinoctialExDot()100%n/a010101
getEquinoctialEy()100%n/a010101
getEquinoctialEyDot()100%n/a010101
getHx()100%n/a010101
getHxDot()100%n/a010101
getHy()100%n/a010101
getHyDot()100%n/a010101
getLv()100%n/a010101
getLvDot()100%n/a010101
getType()100%n/a010101