EcksteinHechlerPropagator

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total20 of 97597%4 of 2483%4432171031
computeMeanParameters(CircularOrbit, double, double, int)1220294%21487%2913401
resetIntermediateState(SpacecraftState, boolean, double, int)82777%1150%121701
toCartesian(AbsoluteDate, UnivariateDerivative2[])208100%n/a0103301
meanToEccentric(UnivariateDerivative2, UnivariateDerivative2, UnivariateDerivative2)84100%1375%1301701
EcksteinHechlerPropagator(Orbit, AttitudeProvider, double, double, double, double, double, double, double, double, PropagationType, double, int)59100%n/a010901
resetInitialState(SpacecraftState, PropagationType, double, int)42100%2100%020701
EcksteinHechlerPropagator(Orbit, AttitudeProvider, double, UnnormalizedSphericalHarmonicsProvider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics, PropagationType)31100%n/a010701
EcksteinHechlerPropagator(Orbit, AttitudeProvider, double, UnnormalizedSphericalHarmonicsProvider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics)30100%n/a010701
computeMeanOrbit(Orbit, UnnormalizedSphericalHarmonicsProvider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics, double, int)29100%n/a010701
computeMeanOrbit(Orbit, double, double, double, double, double, double, double, double, int)23100%n/a010301
propagateOrbit(AbsoluteDate)21100%n/a010301
EcksteinHechlerPropagator(Orbit, AttitudeProvider, double, double, double, double, double, double, double, double, PropagationType)16100%n/a010201
EcksteinHechlerPropagator(Orbit, double, double, double, double, double, double, double)15100%n/a010201
EcksteinHechlerPropagator(Orbit, double, double, double, double, double, double, double, double)15100%n/a010201
EcksteinHechlerPropagator(Orbit, AttitudeProvider, double, double, double, double, double, double, double, double)14100%n/a010201
EcksteinHechlerPropagator(Orbit, UnnormalizedSphericalHarmonicsProvider, PropagationType)14100%n/a010301
EcksteinHechlerPropagator(Orbit, UnnormalizedSphericalHarmonicsProvider)13100%n/a010301
EcksteinHechlerPropagator(Orbit, double, UnnormalizedSphericalHarmonicsProvider)13100%n/a010301
EcksteinHechlerPropagator(Orbit, AttitudeProvider, double, double, double, double, double, double, double)13100%n/a010201
EcksteinHechlerPropagator(Orbit, AttitudeProvider, double, UnnormalizedSphericalHarmonicsProvider, PropagationType)12100%n/a010201
EcksteinHechlerPropagator(Orbit, AttitudeProvider, UnnormalizedSphericalHarmonicsProvider)11100%n/a010201
EcksteinHechlerPropagator(Orbit, AttitudeProvider, double, UnnormalizedSphericalHarmonicsProvider)11100%n/a010201
createHarvester(String, RealMatrix, DoubleArrayDictionary)8100%n/a010101
computeMeanOrbit(Orbit, UnnormalizedSphericalHarmonicsProvider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics)7100%n/a010101
resetInitialState(SpacecraftState, PropagationType)7100%n/a010201
resetIntermediateState(SpacecraftState, boolean)7100%n/a010201
getMass(AbsoluteDate)7100%n/a010101
resetInitialState(SpacecraftState)5100%n/a010201
getCk0()5100%n/a010101
getMu()3100%n/a010101
getReferenceRadius()3100%n/a010101