FieldCircularOrbit

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total44 of 4,47299%5 of 9294%61076570158
normalizeAngle(RealFieldElement, RealFieldElement)160%n/a111111
FieldCircularOrbit(TimeStampedFieldPVCoordinates, Frame, RealFieldElement)1356497%1375%1326801
FieldCircularOrbit(RealFieldElement, RealFieldElement, RealFieldElement, RealFieldElement, RealFieldElement, RealFieldElement, RealFieldElement, RealFieldElement, RealFieldElement, RealFieldElement, RealFieldElement, RealFieldElement, PositionAngle, Frame, FieldAbsoluteDate, RealFieldElement)1016394%21083%2924201
addKeplerContribution(PositionAngle, RealFieldElement, RealFieldElement[])13896%1375%1411401
computeJacobianMeanWrtCartesian()1,111100%n/a01010801
computePVWithoutA()313100%2100%0203801
interpolate(FieldAbsoluteDate, Stream)280100%12100%0704301
FieldCircularOrbit(FieldOrbit)251100%6100%0403901
nonKeplerianAcceleration()203100%n/a0102201
computeJacobianTrueWrtCartesian()190100%2100%0202301
shiftedBy(RealFieldElement)113100%2100%0201701
meanToEccentric(RealFieldElement, RealFieldElement, RealFieldElement)102100%1375%1301701
toOrbit()83100%2100%0201101
computeJacobianEccentricWrtCartesian()79100%2100%0201201
getHxDot()64100%4100%030901
getHyDot()64100%4100%030901
eccentricToTrue(RealFieldElement, RealFieldElement, RealFieldElement)57100%n/a010601
trueToEccentric(RealFieldElement, RealFieldElement, RealFieldElement)57100%n/a010501
toString()50100%n/a010701
initPVCoordinates()49100%2100%020701
getAlphaMDot()42100%2100%020701
getEquinoctialExDot()41100%2100%020601
getEquinoctialEyDot()41100%2100%020601
getAlphaEDot()39100%2100%020701
getHx()28100%2100%020301
getHy()28100%2100%020301
getEDot()23100%2100%020301
FieldCircularOrbit(RealFieldElement, RealFieldElement, RealFieldElement, RealFieldElement, RealFieldElement, RealFieldElement, PositionAngle, Frame, FieldAbsoluteDate, RealFieldElement)19100%n/a010201
getEquinoctialEx()16100%n/a010101
getEquinoctialEy()16100%n/a010101
getE()16100%n/a010101
getAlpha(PositionAngle)15100%4100%030301
getAlphaDot(PositionAngle)15100%4100%030301
eccentricToMean(RealFieldElement, RealFieldElement, RealFieldElement)14100%n/a010101
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, RealFieldElement)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