FieldCircularOrbit

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total28 of 4,75499%5 of 8293%51065581062
FieldCircularOrbit(TimeStampedFieldPVCoordinates, Frame, CalculusFieldElement)1358097%1375%1326401
FieldCircularOrbit(CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, PositionAngleType, Frame, FieldAbsoluteDate, CalculusFieldElement)1015293%21083%2924001
addKeplerContribution(PositionAngleType, CalculusFieldElement, CalculusFieldElement[])15496%1375%1411501
computeJacobianMeanWrtCartesian()1,150100%n/a01011101
computePVWithoutA()331100%2100%0203901
FieldCircularOrbit(FieldOrbit)251100%6100%0403801
initPosition()225100%n/a0102801
nonKeplerianAcceleration()218100%n/a0102201
computeJacobianTrueWrtCartesian()201100%2100%0202401
FieldCircularOrbit(Field, CircularOrbit)139100%2100%0202201
shiftedBy(CalculusFieldElement)115100%2100%0201801
meanToEccentric(CalculusFieldElement, CalculusFieldElement, CalculusFieldElement)104100%1375%1301501
computeJacobianEccentricWrtCartesian()88100%2100%0201301
toOrbit()83100%2100%0201101
getHxDot()68100%4100%030801
getHyDot()68100%4100%030801
eccentricToTrue(CalculusFieldElement, CalculusFieldElement, CalculusFieldElement)66100%n/a010501
trueToEccentric(CalculusFieldElement, CalculusFieldElement, CalculusFieldElement)66100%n/a010401
initPVCoordinates()51100%2100%020801
toString()50100%n/a010701
getAlphaMDot()43100%2100%020701
getEquinoctialExDot()42100%2100%020501
getEquinoctialEyDot()42100%2100%020501
getAlphaEDot()39100%2100%020701
getHx()33100%2100%020301
getHy()33100%2100%020301
removeRates()27100%n/a010401
getEDot()24100%2100%020301
getEquinoctialEx()21100%n/a010201
getEquinoctialEy()21100%n/a010201
eccentricToMean(CalculusFieldElement, CalculusFieldElement, CalculusFieldElement)21100%n/a010201
FieldCircularOrbit(CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, PositionAngleType, Frame, FieldAbsoluteDate, CalculusFieldElement)19100%n/a010201
getE()17100%n/a010101
getAlpha(PositionAngleType)15100%4100%030301
getAlphaDot(PositionAngleType)15100%4100%030301
getAlphaM()13100%n/a010101
getLvDot()12100%2100%020101
getLEDot()12100%2100%020101
getLMDot()12100%2100%020101
FieldCircularOrbit(FieldPVCoordinates, Frame, FieldAbsoluteDate, CalculusFieldElement)10100%n/a010201
FieldCircularOrbit(Field, Orbit)100%n/a010201
getAlphaE()100%n/a010101
shiftedBy(double)100%n/a010101
getLv()100%n/a010101
getLE()100%n/a010101
getLM()100%n/a010101
hasDerivatives()100%2100%020101
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
hasRates()100%n/a010101
getType()100%n/a010101
getCachedPositionAngleType()100%n/a010101