AemWriter

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total87 of 1,74295%16 of 10584%218311274526
writeEulerAngle(XmlGenerator, double, RotationOrder, AbsoluteDate, String[])306167%1150%1231401
writeQuaternionDerivative(XmlGenerator, double, boolean, AbsoluteDate, String[])2214286%9950%91032501
writeQuaternionEulerRates(XmlGenerator, boolean, RotationOrder, AbsoluteDate, String[])1010791%2250%2311901
writeQuaternion(XmlGenerator, double, boolean, AbsoluteDate, String[])108589%2880%2611601
writeAttitudeEphemerisLine(Generator, double, AemMetadata, TimeStampedAngularCoordinates)515596%11493%11313601
lambda$new$7()0%n/a111111
lambda$new$6()0%n/a111111
lambda$new$3()0%n/a111111
lambda$new$1()0%n/a111111
lambda$new$0(IERSConventions)0%n/a111111
writeMetadata(Generator, double, AemMetadata)321100%14397%12304501
writeEulerAngleDerivative(XmlGenerator, double, RotationOrder, AbsoluteDate, String[])165100%4100%0302401
writeQuaternionAngularVelocity(XmlGenerator, AbsoluteDate, String[])103100%n/a0101601
writeSpinNutation(XmlGenerator, AbsoluteDate, String[])89100%n/a0101201
writeSpinNutationMomentum(XmlGenerator, AbsoluteDate, String[])89100%n/a0101201
writeEulerAngleAngularVelocity(XmlGenerator, double, RotationOrder, AbsoluteDate, String[])79100%n/a0101101
writeSpin(XmlGenerator, AbsoluteDate, String[])59100%n/a010901
writeLabeledEulerAngle(XmlGenerator, int, String, String)59100%2100%020701
writeLabeledEulerRate(XmlGenerator, int, String, String)59100%2100%020701
writeSegmentContent(Generator, double, AemSegment)40100%2100%020901
AemWriter(IERSConventions, DataContext, AbsoluteDate)20100%n/a010201
startAttitudeBlock(Generator)12100%2100%020401
endAttitudeBlock(Generator)4100%n/a010201
lambda$new$5()100%n/a010101
lambda$new$4(AbsoluteDate)100%n/a010101
lambda$new$2(DataContext)100%n/a010101