FieldCircularOrbit

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total28 of 4,49699%5 of 9294%51065569057
FieldCircularOrbit(TimeStampedFieldPVCoordinates, Frame, CalculusFieldElement)1356497%1375%1326601
FieldCircularOrbit(CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, PositionAngle, Frame, FieldAbsoluteDate, CalculusFieldElement)1016394%21083%2924201
addKeplerContribution(PositionAngle, CalculusFieldElement, CalculusFieldElement[])14296%1375%1411501
computeJacobianMeanWrtCartesian()1,115100%n/a01011001
computePVWithoutA()316100%2100%0203901
interpolate(FieldAbsoluteDate, Stream)280100%12100%0704301
FieldCircularOrbit(FieldOrbit)253100%6100%0404001
nonKeplerianAcceleration()203100%n/a0102201
computeJacobianTrueWrtCartesian()193100%2100%0202401
shiftedBy(CalculusFieldElement)113100%2100%0201701
meanToEccentric(CalculusFieldElement, CalculusFieldElement, CalculusFieldElement)100100%1375%1301501
toOrbit()83100%2100%0201101
computeJacobianEccentricWrtCartesian()82100%2100%0201301
getHxDot()65100%4100%030801
getHyDot()65100%4100%030801
eccentricToTrue(CalculusFieldElement, CalculusFieldElement, CalculusFieldElement)60100%n/a010501
trueToEccentric(CalculusFieldElement, CalculusFieldElement, CalculusFieldElement)60100%n/a010401
toString()50100%n/a010701
initPVCoordinates()49100%2100%020701
getAlphaMDot()42100%2100%020701
getEquinoctialExDot()39100%2100%020501
getEquinoctialEyDot()39100%2100%020501
getAlphaEDot()39100%2100%020701
getHx()31100%2100%020301
getHy()31100%2100%020301
getEDot()23100%2100%020301
getEquinoctialEx()20100%n/a010201
getEquinoctialEy()20100%n/a010201
FieldCircularOrbit(CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, PositionAngle, Frame, FieldAbsoluteDate, CalculusFieldElement)19100%n/a010201
eccentricToMean(CalculusFieldElement, CalculusFieldElement, CalculusFieldElement)19100%n/a010201
getE()16100%n/a010101
getAlpha(PositionAngle)15100%4100%030301
getAlphaDot(PositionAngle)15100%4100%030301
getAlphaM()13100%n/a010101
getLvDot()12100%2100%020101
getLEDot()12100%2100%020101
getLMDot()12100%2100%020101
shiftedBy(double)11100%n/a010101
FieldCircularOrbit(FieldPVCoordinates, Frame, FieldAbsoluteDate, CalculusFieldElement)10100%n/a010201
getAlphaE()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
getType()100%n/a010101