StateCovariance

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total0 of 557100%0 of 26100%0350112022
shiftedBy(Orbit, double)86100%4100%0301301
changeFrameAndCreate(Orbit, AbsoluteDate, Frame, Frame, RealMatrix, OrbitType, PositionAngle)66100%4100%0301201
changeFrameAndCreate(Orbit, AbsoluteDate, Frame, LOFType, RealMatrix, OrbitType, PositionAngle)57100%2100%0201401
changeTypeAndCreate(Orbit, AbsoluteDate, Frame, OrbitType, PositionAngle, OrbitType, PositionAngle, RealMatrix)55100%n/a0101101
changeFrameAndCreate(Orbit, AbsoluteDate, LOFType, Frame, RealMatrix)51100%2100%0201101
changeCovarianceType(Orbit, OrbitType, PositionAngle)36100%4100%030501
changeCovarianceFrame(Orbit, LOFType)27100%2100%020301
changeCovarianceFrame(Orbit, Frame)27100%2100%020301
getStm(Orbit, double)27100%n/a010601
checkInputConsistency(Frame, OrbitType)26100%6100%040601
StateCovariance(RealMatrix, AbsoluteDate, Frame, LOFType, OrbitType, PositionAngle)25100%n/a010901
changeFrameAndCreate(Orbit, AbsoluteDate, LOFType, LOFType, RealMatrix)21100%n/a010501
getJacobian(Transform)14100%n/a010301
StateCovariance(RealMatrix, AbsoluteDate, LOFType)9100%n/a010201
StateCovariance(RealMatrix, AbsoluteDate, Frame, OrbitType, PositionAngle)9100%n/a010201
getDate()3100%n/a010101
getMatrix()3100%n/a010101
getOrbitType()3100%n/a010101
getPositionAngle()3100%n/a010101
getFrame()3100%n/a010101
getLOFType()3100%n/a010101
static {...}3100%n/a010101