GNSSOrbitalElementsFactory

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total39 of 53292%2 of 666%4427115339
toArray(Orbit)270%20%225511
getJacobianWrtParameters()90%n/a111111
getAngularVelocity()30%n/a111111
jacobianWrtParameters(GNSSOrbitalElements, Frame, Frame)142100%n/a0102901
buildOrbitalDrivers()79100%n/a0101401
GNSSOrbitalElementsFactory(double, TimeScales, SatelliteSystem, String, Frame, Frame, double)54100%n/a0101201
createOrbitFromDrivers()48100%n/a010801
setTimeOfEphemerisNoRecurse(int, double)38100%2100%020601
setDate(AbsoluteDate)11100%n/a010201
setTimeOfClock(GNSSDate)10100%2100%020401
setTimeOfEphemeris(GNSSDate)9100%n/a010301
setPrn(int)4100%n/a010201
getTimeDriver()4100%n/a010101
getADotDriver()4100%n/a010101
getDeltaN0Driver()4100%n/a010101
getDeltaN0DotDriver()4100%n/a010101
getIDotDriver()4100%n/a010101
getOmegaDotDriver()4100%n/a010101
getCucDriver()4100%n/a010101
getCusDriver()4100%n/a010101
getCrcDriver()4100%n/a010101
getCrsDriver()4100%n/a010101
getCicDriver()4100%n/a010101
getCisDriver()4100%n/a010101
getAf0Driver()4100%n/a010101
getAf1Driver()4100%n/a010101
getAf2Driver()4100%n/a010101
setTgd(double)4100%n/a010201
lambda$jacobianWrtParameters$0(double)4100%n/a010101
getInertial()3100%n/a010101
getBodyFixed()3100%n/a010101
getTimeScales()3100%n/a010101
getSystem()3100%n/a010101
getType()3100%n/a010101
getPrn()3100%n/a010101
getTimeOfEphemeris()3100%n/a010101
getTimeOfClock()3100%n/a010101
getNonKeplerianParametersDrivers()3100%n/a010101
getTgd()3100%n/a010101