FieldEcksteinHechlerPropagator

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total54 of 98594%8 of 2466%11347161322
normalizeAngle(RealFieldElement, RealFieldElement)160%n/a111111
FieldEcksteinHechlerPropagator(FieldOrbit, RealFieldElement, double, RealFieldElement, double, double, double, double, double)150%n/a112211
computeMeanParameters(FieldCircularOrbit, RealFieldElement)1224695%61062%6913801
resetIntermediateState(FieldSpacecraftState, boolean)62379%1150%121701
resetInitialState(FieldSpacecraftState)50%n/a112211
toCartesian(FieldAbsoluteDate, FieldUnivariateDerivative2[])208100%n/a0103301
meanToEccentric(FieldUnivariateDerivative2, FieldUnivariateDerivative2, FieldUnivariateDerivative2)85100%1375%1301701
FieldEcksteinHechlerPropagator(FieldOrbit, AttitudeProvider, RealFieldElement, double, RealFieldElement, double, double, double, double, double, PropagationType)66100%n/a0101201
resetInitialState(FieldSpacecraftState, PropagationType)43100%2100%020701
FieldEcksteinHechlerPropagator(FieldOrbit, AttitudeProvider, RealFieldElement, UnnormalizedSphericalHarmonicsProvider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics, PropagationType)38100%n/a010701
FieldEcksteinHechlerPropagator(FieldOrbit, AttitudeProvider, RealFieldElement, UnnormalizedSphericalHarmonicsProvider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics)37100%n/a010701
FieldEcksteinHechlerPropagator(FieldOrbit, double, RealFieldElement, double, double, double, double, double)22100%n/a010301
FieldEcksteinHechlerPropagator(FieldOrbit, UnnormalizedSphericalHarmonicsProvider, PropagationType)22100%n/a010401
FieldEcksteinHechlerPropagator(FieldOrbit, UnnormalizedSphericalHarmonicsProvider)21100%n/a010401
propagateOrbit(FieldAbsoluteDate)21100%n/a010301
FieldEcksteinHechlerPropagator(FieldOrbit, AttitudeProvider, double, RealFieldElement, double, double, double, double, double)20100%n/a010201
FieldEcksteinHechlerPropagator(FieldOrbit, AttitudeProvider, UnnormalizedSphericalHarmonicsProvider)19100%n/a010201
FieldEcksteinHechlerPropagator(FieldOrbit, RealFieldElement, UnnormalizedSphericalHarmonicsProvider)14100%n/a010301
FieldEcksteinHechlerPropagator(FieldOrbit, AttitudeProvider, RealFieldElement, double, RealFieldElement, double, double, double, double, double)14100%n/a010201
FieldEcksteinHechlerPropagator(FieldOrbit, AttitudeProvider, RealFieldElement, UnnormalizedSphericalHarmonicsProvider, PropagationType)13100%n/a010201
FieldEcksteinHechlerPropagator(FieldOrbit, AttitudeProvider, RealFieldElement, UnnormalizedSphericalHarmonicsProvider)12100%n/a010201
getMass(FieldAbsoluteDate)7100%n/a010101