FieldCircularOrbit

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total40 of 4,85399%11 of 10289%111228592064
initializeCachedAlpha(CalculusFieldElement, CalculusFieldElement, PositionAngleType)8394%11191%1811601
getAlphaVDot()7593%1375%1411301
getAlphaEDot()7593%1375%1411301
getAlphaMDot()7593%1375%1411301
withFrame(Frame)3788%1375%131801
getAlphaV()2583%1375%141501
getAlphaE()2583%1375%141501
getAlphaM()2583%1375%141501
computeJacobianMeanWrtCartesian()1,144100%n/a01011101
FieldCircularOrbit(TimeStampedFieldPVCoordinates, Frame, CalculusFieldElement)608100%4100%0306501
computePVWithoutA()329100%2100%0203901
FieldCircularOrbit(FieldOrbit)271100%6100%0403901
initPosition()223100%n/a0102801
nonKeplerianAcceleration()218100%n/a0102201
computeJacobianTrueWrtCartesian()201100%2100%0202401
FieldCircularOrbit(Field, CircularOrbit)125100%n/a0101601
shiftedBy(CalculusFieldElement)116100%2100%0201801
computeKeplerianAlphaDot(PositionAngleType, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, PositionAngleType)113100%4100%0301201
computeJacobianEccentricWrtCartesian()88100%2100%0201301
FieldCircularOrbit(CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, PositionAngleType, PositionAngleType, Frame, FieldAbsoluteDate, CalculusFieldElement)83100%2100%0202001
getHxDot()69100%4100%030801
getHyDot()69100%4100%030801
hasNonKeplerianAcceleration()58100%3975%370201
toOrbit()52100%n/a010701
initPVCoordinates()51100%2100%020801
toString()50100%n/a010701
getEquinoctialExDot()43100%2100%020501
getEquinoctialEyDot()43100%2100%020501
FieldCircularOrbit(CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, PositionAngleType, PositionAngleType, Frame, FieldAbsoluteDate, CalculusFieldElement)42100%n/a010401
withCachedPositionAngleType(PositionAngleType)37100%n/a010201
getHx()33100%2100%020301
getHy()33100%2100%020301
withKeplerianRates()24100%n/a010301
addKeplerContribution(PositionAngleType, CalculusFieldElement, CalculusFieldElement[])22100%n/a010201
getEquinoctialEx()21100%n/a010201
getEquinoctialEy()21100%n/a010201
FieldCircularOrbit(CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, PositionAngleType, Frame, FieldAbsoluteDate, CalculusFieldElement)20100%n/a010201
getEDot()19100%n/a010101
getE()17100%n/a010101
getAlpha(PositionAngleType)15100%4100%030301
getAlphaDot(PositionAngleType)15100%4100%030301
FieldCircularOrbit(CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, PositionAngleType, Frame, FieldAbsoluteDate, CalculusFieldElement)14100%n/a010201
FieldCircularOrbit(FieldPVCoordinates, Frame, FieldAbsoluteDate, CalculusFieldElement)10100%n/a010201
FieldCircularOrbit(Field, Orbit)100%n/a010201
shiftedBy(double)100%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
getA()100%n/a010101
getADot()100%n/a010101
getCircularEx()100%n/a010101
getCircularExDot()100%n/a010101
getCircularEy()100%n/a010101
getCircularEyDot()100%n/a010101
getI()100%n/a010101
getIDot()100%n/a010101
getRightAscensionOfAscendingNode()100%n/a010101
getRightAscensionOfAscendingNodeDot()100%n/a010101
getCachedPositionAngleType()100%n/a010101
hasNonKeplerianRates()100%n/a010101
getType()100%n/a010101