AEMFile.AttitudeEphemeridesBlock

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total0 of 168100%0 of 4100%041063039
AEMFile.AttitudeEphemeridesBlock(AEMFile)17100%n/a010401
getStart()10100%2100%020401
getStop()10100%2100%020401
setAttitudeDataLinesComment(List)7100%n/a010201
getTimeScaleString()5100%n/a010101
getAngularCoordinates()4100%n/a010101
getFrameCenterString()4100%n/a010101
setRefFrameAString(String)4100%n/a010201
setRefFrameBString(String)4100%n/a010201
setRateFrameString(String)4100%n/a010201
setAttitudeDirection(String)4100%n/a010201
setAttitudeType(String)4100%n/a010201
setIsFirst(boolean)4100%n/a010201
setEulerRotSeq(String)4100%n/a010201
getTimeScale()4100%n/a010101
setStartTime(AbsoluteDate)4100%n/a010201
setStopTime(AbsoluteDate)4100%n/a010201
setUseableStartTime(AbsoluteDate)4100%n/a010201
setUseableStopTime(AbsoluteDate)4100%n/a010201
setInterpolationMethod(String)4100%n/a010201
setInterpolationDegree(int)4100%n/a010201
setRotationOrder(RotationOrder)4100%n/a010201
getAttitudeDataLines()3100%n/a010101
getMetaData()3100%n/a010101
getRefFrameAString()3100%n/a010101
getRefFrameBString()3100%n/a010101
getRateFrameString()3100%n/a010101
getAttitudeDirection()3100%n/a010101
getAttitudeType()3100%n/a010101
isFirst()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
getAttitudeDataLinesComment()3100%n/a010101
getRotationOrder()3100%n/a010101