Position

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total66 of 46485%1 of 1492%7231254616
Position(AbsoluteDate, Vector3D, double, double)110%n/a112211
Position(AbsoluteDate, Vector3D, double, double, int)110%n/a112211
Position(AbsoluteDate, Vector3D, double[], double)110%n/a112211
Position(AbsoluteDate, Vector3D, double[], double, int)110%n/a112211
Position(AbsoluteDate, Vector3D, double[][], double)110%n/a112211
Position(AbsoluteDate, Vector3D, double[][], double, int)110%n/a112211
static {...}91100%n/a010101
extractSigmas(double[][])61100%1583%140801
theoreticalEvaluation(int, int, SpacecraftState[])56100%n/a010801
buildPvCovarianceMatrix(double[])48100%4100%030601
Position(AbsoluteDate, Vector3D, double[][], double, ObservableSatellite)47100%n/a010601
getCorrelationCoefficientsMatrix()46100%4100%030601
Position(AbsoluteDate, Vector3D, double, double, ObservableSatellite)21100%n/a010201
getPosition()16100%n/a010201
Position(AbsoluteDate, Vector3D, double[], double, ObservableSatellite)9100%n/a010201
getCovarianceMatrix()3100%n/a010101