FieldEquinoctialOrbit

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total44 of 3,49498%5 of 6692%6826441146
normalizeAngle(RealFieldElement, RealFieldElement)160%n/a111111
FieldEquinoctialOrbit(TimeStampedFieldPVCoordinates, Frame, RealFieldElement)1348597%1375%1325801
FieldEquinoctialOrbit(RealFieldElement, RealFieldElement, RealFieldElement, RealFieldElement, RealFieldElement, RealFieldElement, RealFieldElement, RealFieldElement, RealFieldElement, RealFieldElement, RealFieldElement, RealFieldElement, PositionAngle, Frame, FieldAbsoluteDate, RealFieldElement)1016794%21083%2924301
addKeplerContribution(PositionAngle, RealFieldElement, RealFieldElement[])13696%1375%1411401
computeJacobianMeanWrtCartesian()672100%n/a0105701
computePVWithoutA()315100%2100%0203401
interpolate(FieldAbsoluteDate, Stream)265100%12100%0703901
nonKeplerianAcceleration()203100%n/a0102201
computeJacobianTrueWrtCartesian()189100%2100%0202301
shiftedBy(RealFieldElement)113100%2100%0201701
meanToEccentric(RealFieldElement, RealFieldElement, RealFieldElement)102100%1375%1301701
toOrbit()83100%2100%0201101
computeJacobianEccentricWrtCartesian()75100%2100%0201101
FieldEquinoctialOrbit(FieldOrbit)74100%n/a0101701
eccentricToTrue(RealFieldElement, RealFieldElement, RealFieldElement)62100%n/a010601
trueToEccentric(RealFieldElement, RealFieldElement, RealFieldElement)62100%n/a010601
initPVCoordinates()49100%2100%020701
toString()48100%n/a010601
getIDot()47100%2100%020501
getLMDot()42100%2100%020701
getLEDot()39100%2100%020701
getEDot()35100%2100%020301
getI()21100%n/a010101
FieldEquinoctialOrbit(RealFieldElement, RealFieldElement, RealFieldElement, RealFieldElement, RealFieldElement, RealFieldElement, PositionAngle, Frame, FieldAbsoluteDate, RealFieldElement)19100%n/a010201
getE()16100%n/a010101
getL(PositionAngle)15100%4100%030301
getLDot(PositionAngle)15100%4100%030301
eccentricToMean(RealFieldElement, RealFieldElement, RealFieldElement)14100%n/a010101
getLM()13100%n/a010101
shiftedBy(double)11100%n/a010101
FieldEquinoctialOrbit(FieldPVCoordinates, Frame, FieldAbsoluteDate, RealFieldElement)10100%n/a010201
getLE()8100%n/a010101
hasDerivatives()7100%2100%020101
getA()100%n/a010101
getADot()100%n/a010101
getEquinoctialEx()100%n/a010101
getEquinoctialExDot()100%n/a010101
getEquinoctialEy()100%n/a010101
getEquinoctialEyDot()100%n/a010101
getHx()100%n/a010101
getHxDot()100%n/a010101
getHy()100%n/a010101
getHyDot()100%n/a010101
getLv()100%n/a010101
getLvDot()100%n/a010101
getType()100%n/a010101