AemMetadata

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total0 of 378100%1 of 2896%145095031
copy(double)99100%1375%1302101
checkMandatoryEntriesExceptDatesAndExternalFrame(double)70100%14100%0801301
validate(double)48100%4100%030901
AemMetadata(int, CcsdsFrameMapper)13100%n/a010401
rateFrameIsA()11100%4100%030101
isSpacecraftBodyRate()9100%n/a010101
isFirst()8100%2100%020101
setRateFrameIsA(boolean)7100%n/a010301
setIsFirst(boolean)7100%n/a010301
getStart()7100%n/a010101
getStop()7100%n/a010101
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
setAngvelFrame(FrameFacade)4100%n/a010201
getFrameAngvelFrame()4100%n/a010101
getEulerRotSeq()4100%n/a010101
getUseableStartTime()4100%n/a010101
getUseableStopTime()4100%n/a010101
getInterpolationMethod()4100%n/a010101
getEndpoints()3100%n/a010101
getAttitudeType()3100%n/a010101
getStartTime()3100%n/a010101
getStopTime()3100%n/a010101
getInterpolationDegree()3100%n/a010101