modify(EstimatedMeasurement) | | 100% | | 93% | 1 | 9 | 0 | 37 | 0 | 1 |
modifyWithoutDerivatives(EstimatedMeasurementBase) | | 100% | | n/a | 0 | 1 | 0 | 8 | 0 | 1 |
phaseErrorIonosphericModel(GroundStation, SpacecraftState) | | 100% | | n/a | 0 | 1 | 0 | 4 | 0 | 1 |
phaseErrorIonosphericModel(GroundStation, FieldSpacecraftState, CalculusFieldElement[]) | | 100% | | n/a | 0 | 1 | 0 | 4 | 0 | 1 |
phaseErrorParameterDerivative(GroundStation, ParameterDriver, SpacecraftState) | | 100% | | n/a | 0 | 1 | 0 | 4 | 0 | 1 |
phaseErrorJacobianState(double[], int) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
PhaseIonosphericDelayModifier(IonosphericModel, double) | | 100% | | n/a | 0 | 1 | 0 | 4 | 0 | 1 |
phaseErrorParameterDerivative(double[], int) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
lambda$phaseErrorParameterDerivative$0(GroundStation, SpacecraftState, ParameterDriver, AbsoluteDate) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getParametersDrivers() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |