Orbit

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total18 of 93898%4 of 5092%5544159127
hasNonKeplerianAcceleration()60%n/a111111
getJacobianWrtParameters(PositionAngleType, double[][])57093%21083%2811901
getJacobianWrtCartesian(PositionAngleType, double[][])56793%11191%1811901
hasNonKeplerianAcceleration(PVCoordinates, double)24195%1583%1411201
fillHalfRow(double, Vector3D, double, Vector3D, double, Vector3D, double, Vector3D, double, Vector3D, double, Vector3D, double[], int)143100%n/a010801
fillHalfRow(double, Vector3D, double, Vector3D, double, Vector3D, double, Vector3D, double, Vector3D, double[], int)124100%n/a010801
Orbit(TimeStampedPVCoordinates, Frame, double)54100%2100%0201501
nonKeplerianAcceleration()54100%n/a0101001
fillHalfRow(double, Vector3D, double, Vector3D, double, Vector3D, double, Vector3D, double[], int)53100%n/a010401
fillHalfRow(double, Vector3D, double, Vector3D, double, Vector3D, double[], int)44100%n/a010401
Orbit(Frame, AbsoluteDate, double)35100%n/a0101301
fillHalfRow(double, Vector3D, double, Vector3D, double[], int)35100%n/a010401
getPVCoordinates(Frame)26100%4100%030601
getPosition(Frame)26100%4100%030601
fillHalfRow(double, Vector3D, double[], int)26100%n/a010401
createInverseJacobian(PositionAngleType)19100%n/a010501
getKeplerianPeriod()18100%2100%020201
ensurePseudoInertialFrame(Frame)16100%2100%020401
getPVCoordinates()15100%2100%020401
getKeplerianMeanMotion()12100%n/a010201
getPosition()10100%2100%020301
isElliptical()9100%2100%020101
getMeanAnomalyDotWrtA()8100%n/a010101
getDecompositionSolver(RealMatrix)6100%n/a010101
getFrame()3100%n/a010101
getMu()3100%n/a010101
getDate()3100%n/a010101