KeplerianAnomalyUtility

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total36 of 96996%5 of 6492%5544155020
hyperbolicMeanToEccentric(double, double)1227095%11191%1724601
hyperbolicMeanToEccentricDifference(double, double, double)127586%2675%2511301
ellipticMeanToEccentricDifference(double, double, double)126183%2675%2511301
ellipticMeanToEccentric(double, double)198100%10100%0602701
eMeSinE(double, double)47100%2100%0201001
ellipticEccentricToTrue(double, double)33100%n/a010301
ellipticTrueToEccentric(double, double)31100%n/a010301
getTrueAnomaly(double, double, PositionAngleType)31100%7100%050401
getEccentricAnomaly(double, double, PositionAngleType)31100%7100%050401
getMeanAnomaly(double, double, PositionAngleType)31100%7100%050401
hyperbolicTrueToEccentric(double, double)23100%n/a010301
convertAnomaly(PositionAngleType, double, double, PositionAngleType)20100%3100%030401
hyperbolicEccentricToTrue(double, double)17100%n/a010101
static {...}11100%n/a010601
ellipticMeanToTrue(double, double)10100%n/a010301
ellipticTrueToMean(double, double)10100%n/a010301
hyperbolicMeanToTrue(double, double)10100%n/a010301
hyperbolicTrueToMean(double, double)10100%n/a010301
ellipticEccentricToMean(double, double)7100%n/a010101
hyperbolicEccentricToMean(double, double)7100%n/a010101