StateCovariance

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total4 of 63399%4 of 5092%3490119024
changeCovarianceType(Orbit, OrbitType, PositionAngleType)47094%3975%270901
shiftedBy(Orbit, double)85100%4100%0301301
changeTypeAndCreate(Orbit, AbsoluteDate, Frame, OrbitType, PositionAngleType, OrbitType, PositionAngleType, RealMatrix)74100%4100%0301401
changeFrameAndCreate(Orbit, AbsoluteDate, Frame, LOF, RealMatrix, OrbitType, PositionAngleType)57100%2100%0201401
changeFrameAndCreate(Orbit, AbsoluteDate, Frame, Frame, RealMatrix, OrbitType, PositionAngleType)57100%4100%0301001
changeFrameAndCreate(Orbit, AbsoluteDate, LOF, Frame, RealMatrix)51100%2100%0201101
changeCovarianceFrame(Orbit, Frame)45100%4100%030501
changeCovarianceFrame(Orbit, LOF)41100%4100%030501
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
inputAndOutputAreIdentical(OrbitType, PositionAngleType, OrbitType, PositionAngleType)10100%1375%130101
inputAndOutputOrbitTypesAreCartesian(OrbitType, OrbitType)10100%4100%030101
StateCovariance(RealMatrix, AbsoluteDate, LOF)9100%n/a010201
StateCovariance(RealMatrix, AbsoluteDate, Frame, OrbitType, PositionAngleType)9100%n/a010201
getJacobian(KinematicTransform)4100%n/a010101
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