FieldCircularOrbit

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total39 of 5,12999%6 of 10094%61137614060
FieldCircularOrbit(TimeStampedFieldPVCoordinates, Frame, double)1364698%1583%1427101
circularToPosition(RealFieldElement, RealFieldElement, RealFieldElement, RealFieldElement, RealFieldElement, RealFieldElement, double)1127796%1150%1223201
FieldCircularOrbit(RealFieldElement, RealFieldElement, RealFieldElement, RealFieldElement, RealFieldElement, RealFieldElement, RealFieldElement, RealFieldElement, RealFieldElement, RealFieldElement, RealFieldElement, RealFieldElement, PositionAngle, Frame, FieldAbsoluteDate, double)1021395%21285%21024501
addKeplerContribution(PositionAngle, double, RealFieldElement[])15496%1375%1411401
computeJacobianMeanWrtCartesian()1,143100%n/a01010801
computePVWithoutA()328100%2100%0203801
FieldCircularOrbit(FieldOrbit)283100%8100%0504101
interpolate(FieldAbsoluteDate, Stream)281100%12100%0704301
nonKeplerianAcceleration()218100%n/a0102201
computeJacobianTrueWrtCartesian()198100%2100%0202301
shiftedBy(RealFieldElement)114100%2100%0201701
meanToEccentric(RealFieldElement, RealFieldElement, RealFieldElement)106100%1375%1301701
computeJacobianEccentricWrtCartesian()85100%2100%0201201
toOrbit()81100%2100%0201101
getAlphaMDot()76100%2100%020801
getAlphaEDot()72100%2100%020801
getHxDot()66100%4100%030901
getHyDot()66100%4100%030901
eccentricToTrue(RealFieldElement, RealFieldElement, RealFieldElement)63100%n/a010601
trueToEccentric(RealFieldElement, RealFieldElement, RealFieldElement)63100%n/a010501
initPVCoordinates()50100%2100%020801
toString()50100%n/a010701
getEquinoctialExDot()44100%2100%020601
getEquinoctialEyDot()44100%2100%020601
getHx()29100%2100%020301
getHy()29100%2100%020301
getEDot()24100%2100%020301
FieldCircularOrbit(RealFieldElement, RealFieldElement, RealFieldElement, RealFieldElement, RealFieldElement, RealFieldElement, PositionAngle, Frame, FieldAbsoluteDate, double)19100%n/a010201
getEquinoctialEx()19100%n/a010101
getEquinoctialEy()19100%n/a010101
eccentricToMean(RealFieldElement, RealFieldElement, RealFieldElement)18100%n/a010101
getE()17100%n/a010101
normalizeAngle(RealFieldElement, RealFieldElement)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, double)10100%n/a010201
getAlphaE()100%n/a010101
getLv()100%n/a010101
getLE()100%n/a010101
getLM()100%n/a010101
hasDerivatives()100%2100%020101
static {...}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
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