FieldBrouwerLyddanePropagator

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total11 of 76698%2 of 2090%3392127129
resetIntermediateState(FieldSpacecraftState, boolean, double, int)62580%1150%121701
getM2(AbsoluteDate)50%n/a111111
computeMeanParameters(FieldKeplerianOrbit, CalculusFieldElement, double, int)256100%11593%1903601
FieldBrouwerLyddanePropagator(FieldOrbit, AttitudeProvider, CalculusFieldElement, double, CalculusFieldElement, double, double, double, double, PropagationType, double, double, int)67100%n/a0101001
resetInitialState(FieldSpacecraftState, PropagationType, double, int)45100%2100%020701
FieldBrouwerLyddanePropagator(FieldOrbit, AttitudeProvider, CalculusFieldElement, UnnormalizedSphericalHarmonicsProvider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics, PropagationType, double)32100%n/a010601
FieldBrouwerLyddanePropagator(FieldOrbit, AttitudeProvider, CalculusFieldElement, UnnormalizedSphericalHarmonicsProvider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics, double)31100%n/a010601
computeMeanOrbit(FieldOrbit, double, double, double, double, double, double, double, double, int)31100%n/a010501
computeMeanOrbit(FieldOrbit, UnnormalizedSphericalHarmonicsProvider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics, double, double, int)26100%n/a010601
FieldBrouwerLyddanePropagator(FieldOrbit, UnnormalizedSphericalHarmonicsProvider, PropagationType, double)20100%n/a010401
FieldBrouwerLyddanePropagator(FieldOrbit, UnnormalizedSphericalHarmonicsProvider, double)19100%n/a010401
FieldBrouwerLyddanePropagator(FieldOrbit, double, CalculusFieldElement, double, double, double, double, double)19100%n/a010301
FieldBrouwerLyddanePropagator(FieldOrbit, AttitudeProvider, UnnormalizedSphericalHarmonicsProvider, double)17100%n/a010301
FieldBrouwerLyddanePropagator(FieldOrbit, AttitudeProvider, double, CalculusFieldElement, double, double, double, double, double)17100%n/a010201
FieldBrouwerLyddanePropagator(FieldOrbit, AttitudeProvider, CalculusFieldElement, double, CalculusFieldElement, double, double, double, double, PropagationType, double)16100%n/a010201
FieldBrouwerLyddanePropagator(FieldOrbit, CalculusFieldElement, UnnormalizedSphericalHarmonicsProvider, double)15100%n/a010301
FieldBrouwerLyddanePropagator(FieldOrbit, CalculusFieldElement, double, CalculusFieldElement, double, double, double, double, double)15100%n/a010201
FieldBrouwerLyddanePropagator(FieldOrbit, AttitudeProvider, CalculusFieldElement, double, CalculusFieldElement, double, double, double, double, double)14100%n/a010201
FieldBrouwerLyddanePropagator(FieldOrbit, AttitudeProvider, CalculusFieldElement, UnnormalizedSphericalHarmonicsProvider, PropagationType, double)14100%n/a010201
FieldBrouwerLyddanePropagator(FieldOrbit, AttitudeProvider, CalculusFieldElement, UnnormalizedSphericalHarmonicsProvider, double)13100%n/a010201
propagateOrbit(FieldAbsoluteDate, CalculusFieldElement[])11100%n/a010201
static {...}10100%n/a010201
computeMeanOrbit(FieldOrbit, UnnormalizedSphericalHarmonicsProvider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics, double)8100%n/a010101
resetInitialState(FieldSpacecraftState, PropagationType)7100%n/a010201
resetIntermediateState(FieldSpacecraftState, boolean)7100%n/a010201
getMass(FieldAbsoluteDate)7100%n/a010101
resetInitialState(FieldSpacecraftState)5100%n/a010201
getM2()4100%n/a010101
getParametersDrivers()4100%n/a010101