StateCovariance

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total0 of 581100%1 of 3497%1390114022
shiftedBy(Orbit, double)85100%4100%0301301
changeCovarianceType(Orbit, OrbitType, PositionAngleType)74100%11191%170901
changeFrameAndCreate(Orbit, AbsoluteDate, Frame, Frame, RealMatrix, OrbitType, PositionAngleType)66100%4100%0301201
changeFrameAndCreate(Orbit, AbsoluteDate, Frame, LOF, RealMatrix, OrbitType, PositionAngleType)57100%2100%0201401
changeTypeAndCreate(Orbit, AbsoluteDate, Frame, OrbitType, PositionAngleType, OrbitType, PositionAngleType, RealMatrix)55100%n/a0101101
changeFrameAndCreate(Orbit, AbsoluteDate, LOF, Frame, RealMatrix)51100%2100%0201101
changeCovarianceFrame(Orbit, LOF)27100%2100%020301
changeCovarianceFrame(Orbit, Frame)27100%2100%020301
checkFrameAndOrbitTypeConsistency(Frame, OrbitType)26100%6100%040601
StateCovariance(RealMatrix, AbsoluteDate, Frame, LOF, OrbitType, PositionAngleType)24100%n/a010901
changeFrameAndCreate(Orbit, AbsoluteDate, LOF, LOF, RealMatrix)21100%n/a010501
getStm(Orbit, double)15100%n/a010401
getJacobian(Transform)14100%n/a010301
StateCovariance(RealMatrix, AbsoluteDate, LOF)9100%n/a010201
StateCovariance(RealMatrix, AbsoluteDate, Frame, OrbitType, PositionAngleType)9100%n/a010201
getDate()3100%n/a010101
getMatrix()3100%n/a010101
getOrbitType()3100%n/a010101
getPositionAngleType()3100%n/a010101
getFrame()3100%n/a010101
getLOF()3100%n/a010101
static {...}3100%n/a010101