AemWriter

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total72 of 1,16093%10 of 6785%15589192522
writeQuaternionDerivative(XmlGenerator, boolean, AbsoluteDate, String[])2012085%4450%4522301
writeMetadata(Generator, AemMetadata)1727594%13196%11723901
writeQuaternionRate(XmlGenerator, boolean, RotationOrder, AbsoluteDate, String[])1010691%2250%2311901
writeQuaternion(XmlGenerator, boolean, AbsoluteDate, String[])106286%2250%2311201
writeAttitudeEphemerisLine(Generator, AemMetadata, TimeStampedAngularCoordinates)512296%11090%1913001
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$0(IERSConventions)0%n/a111111
writeEulerAngleRate(XmlGenerator, RotationOrder, AbsoluteDate, String[])92100%n/a0101501
writeEulerAngle(XmlGenerator, int, String, String)59100%2100%020701
writeEulerRate(XmlGenerator, int, String, String)59100%2100%020701
writeSpin(XmlGenerator, AbsoluteDate, String[])58100%n/a010901
writeEulerAngle(XmlGenerator, RotationOrder, AbsoluteDate, String[])55100%n/a0101001
writeSegmentContent(Generator, double, AemSegment)38100%2100%020901
AemWriter(IERSConventions, DataContext, AbsoluteDate)20100%n/a010201
startAttitudeBlock(Generator)12100%2100%020401
endAttitudeBlock(Generator)4100%n/a010201
lambda$new$5()100%n/a010101
lambda$new$4(AbsoluteDate)100%n/a010101
lambda$new$2(DataContext)100%n/a010101