AEMFile

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total0 of 131100%0 of 8100%0902505
getSatellites()66100%4100%0301201
checkTimeSystems()44100%4100%030701
addAttitudeBlock()9100%n/a010201
AEMFile()8100%n/a010301
getAttitudeBlocks()4100%n/a010101