APMFile

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total0 of 339100%0 of 2100%0770122076
APMFile()50100%n/a0101201
getHasManeuver()8100%2100%020101
setEpochComment(List)7100%n/a010201
setEulerComment(List)7100%n/a010201
setSpinComment(List)7100%n/a010201
setSpacecraftComment(List)7100%n/a010201
getManeuver(int)6100%n/a010101
addManeuver(APMFile.APMManeuver)6100%n/a010201
setEpoch(AbsoluteDate)4100%n/a010201
setQuaternionFrameAString(String)4100%n/a010201
setQuaternionFrameBString(String)4100%n/a010201
setAttitudeQuaternionDirection(String)4100%n/a010201
setQuaternion(Quaternion)4100%n/a010201
setQuaternionDot(Quaternion)4100%n/a010201
setEulerFrameAString(String)4100%n/a010201
setEulerFrameBString(String)4100%n/a010201
setEulerDirection(String)4100%n/a010201
setEulerRotSeq(String)4100%n/a010201
setRateFrameString(String)4100%n/a010201
setRotationAngles(Vector3D)4100%n/a010201
setRotationRates(Vector3D)4100%n/a010201
setSpinFrameAString(String)4100%n/a010201
setSpinFrameBString(String)4100%n/a010201
setSpinDirection(String)4100%n/a010201
setSpinAlpha(double)4100%n/a010201
setSpinDelta(double)4100%n/a010201
setSpinAngle(double)4100%n/a010201
setSpinAngleVel(double)4100%n/a010201
setNutation(double)4100%n/a010201
setNutationPeriod(double)4100%n/a010201
setNutationPhase(double)4100%n/a010201
setInertiaRefFrameString(String)4100%n/a010201
setI11(double)4100%n/a010201
setI22(double)4100%n/a010201
setI33(double)4100%n/a010201
setI12(double)4100%n/a010201
setI13(double)4100%n/a010201
setI23(double)4100%n/a010201
getEpochComment()4100%n/a010101
getEulerComment()4100%n/a010101
getSpinComment()4100%n/a010101
getSpacecraftComment()4100%n/a010101
getNbManeuvers()4100%n/a010101
getManeuvers()4100%n/a010101
getMetaDataComment()4100%n/a010101
getMetaData()3100%n/a010101
getEpoch()3100%n/a010101
getQuaternionFrameAString()3100%n/a010101
getQuaternionFrameBString()3100%n/a010101
getAttitudeQuaternionDirection()3100%n/a010101
getQuaternion()3100%n/a010101
getQuaternionDot()3100%n/a010101
getEulerFrameAString()3100%n/a010101
getEulerFrameBString()3100%n/a010101
getEulerDirection()3100%n/a010101
getEulerRotSeq()3100%n/a010101
getRateFrameString()3100%n/a010101
getRotationAngles()3100%n/a010101
getRotationRates()3100%n/a010101
getSpinFrameAString()3100%n/a010101
getSpinFrameBString()3100%n/a010101
getSpinDirection()3100%n/a010101
getSpinAlpha()3100%n/a010101
getSpinDelta()3100%n/a010101
getSpinAngle()3100%n/a010101
getSpinAngleVel()3100%n/a010101
getNutation()3100%n/a010101
getNutationPeriod()3100%n/a010101
getNutationPhase()3100%n/a010101
getInertiaRefFrameString()3100%n/a010101
getI11()3100%n/a010101
getI22()3100%n/a010101
getI33()3100%n/a010101
getI12()3100%n/a010101
getI13()3100%n/a010101
getI23()3100%n/a010101