AemMetadata

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total4 of 32598%2 of 3494%246192029
copy(double)49095%2880%2612201
checkMandatoryEntriesExceptDatesAndExternalFrame(double)58100%14100%0801001
validate(double)19100%n/a010501
isSpacecraftBodyRate()12100%2100%020101
AemMetadata(int)11100%n/a010401
getStart()10100%2100%020401
getStop()10100%2100%020401
rateFrameIsA()9100%2100%020101
isFirst()8100%2100%020101
setRateFrameIsA(boolean)7100%n/a010301
setIsFirst(boolean)7100%n/a010301
setAttitudeType(AttitudeType)6100%n/a010301
setEulerRotSeq(RotationOrder)6100%n/a010301
setStartTime(AbsoluteDate)6100%n/a010301
setStopTime(AbsoluteDate)6100%n/a010301
setUseableStartTime(AbsoluteDate)6100%n/a010301
setUseableStopTime(AbsoluteDate)6100%n/a010301
setInterpolationMethod(String)6100%n/a010301
setInterpolationDegree(int)6100%n/a010301
getInterpolationSamples()5100%n/a010101
getEndpoints()3100%n/a010101
getAttitudeType()3100%n/a010101
getEulerRotSeq()3100%n/a010101
getStartTime()3100%n/a010101
getStopTime()3100%n/a010101
getUseableStartTime()3100%n/a010101
getUseableStopTime()3100%n/a010101
getInterpolationMethod()3100%n/a010101
getInterpolationDegree()3100%n/a010101