PV

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total47 of 78093%5 of 3284%531473015
buildPvCovarianceMatrix(double[][], double[][])299376%3975%3731401
buildPvCovarianceMatrix(double[], double[])186879%1583%141901
static {...}178100%n/a010101
PV(AbsoluteDate, Vector3D, Vector3D, double[][], double, ObservableSatellite)71100%n/a010701
theoreticalEvaluation(int, int, SpacecraftState[])65100%n/a010701
extractSigmas(double[][])61100%1583%140801
buildPvCovarianceMatrix(double[])48100%4100%030601
getCorrelationCoefficientsMatrix()46100%4100%030601
PV(AbsoluteDate, Vector3D, Vector3D, double, double, double, ObservableSatellite)34100%n/a010201
getPosition()16100%n/a010201
getVelocity()16100%n/a010201
PV(AbsoluteDate, Vector3D, Vector3D, double[], double[], double, ObservableSatellite)11100%n/a010301
PV(AbsoluteDate, Vector3D, Vector3D, double[][], double[][], double, ObservableSatellite)11100%n/a010301
PV(AbsoluteDate, Vector3D, Vector3D, double[], double, ObservableSatellite)10100%n/a010201
getCovarianceMatrix()5100%n/a010101