GNSSOrbitalElements

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total0 of 520100%0 of 0n/a0320112032
toField(Field)145100%n/a0101801
factory(Frame, Frame)137100%n/a0102601
GNSSOrbitalElements(double, int, TimeScales, String, int, GNSSDate, KeplerianOrbit, double, double, double, double, double, double, double, double, double, double, double, double, double, double, double, GNSSDate)72100%n/a0102501
GNSSOrbitalElements(FieldGnssOrbitalElements)67100%n/a0101201
reset(GNSSOrbitalElementsFactory, String, ToDoubleFunction)11100%n/a010201
reset(ParameterDriver, double)7100%n/a010301
getCycleDuration()6100%n/a010101
getDate()4100%n/a010101
getTimeOfEphemeris()3100%n/a010101
getTimeOfClock()3100%n/a010101
getTimeScales()3100%n/a010101
getType()3100%n/a010101
getAngularVelocity()3100%n/a010101
getWeeksInCycle()3100%n/a010101
getPrn()3100%n/a010101
getOrbit()3100%n/a010101
getADot()3100%n/a010101
getDeltaN0()3100%n/a010101
getDeltaN0Dot()3100%n/a010101
getIDot()3100%n/a010101
getOmegaDot()3100%n/a010101
getCuc()3100%n/a010101
getCus()3100%n/a010101
getCrc()3100%n/a010101
getCrs()3100%n/a010101
getCic()3100%n/a010101
getCis()3100%n/a010101
getAf0()3100%n/a010101
getAf1()3100%n/a010101
getAf2()3100%n/a010101
getTgd()3100%n/a010101
isCivilianMessage()2100%n/a010101