GLONASSNumericalPropagator

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total55 of 1,09394%4 of 1471%4218200014
getEccentricAnomaly(double, double)3416482%3770%3642701
eMeSinE(double, double)212655%1150%1241001
computeMoonElements(GLONASSDate)280100%n/a0104601
computeSunElements(GLONASSDate)150100%n/a0102901
getPVInPZ90(SpacecraftState)132100%n/a0102601
getPVInInertial(GLONASSDate)106100%n/a0101401
GLONASSNumericalPropagator(ClassicalRungeKuttaIntegrator, GLONASSOrbitalElements, Frame, AttitudeProvider, double, DataContext, boolean)57100%2100%0201901
propagate(AbsoluteDate)47100%n/a0101101
setInitialState()25100%n/a010501
getTrueAnomaly(double, double)22100%n/a010401
static {...}11100%n/a010601
createMapper(AbsoluteDate, double, OrbitType, PositionAngleType, AttitudeProvider, Frame)10100%n/a010101
getMainStateEquations(ODEIntegrator)5100%n/a010101
getGLONASSOrbitalElements()3100%n/a010101