| 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 |
| phaseErrorParameterDerivative(double[], int) | | 100% | | 100% | 0 | 2 | 0 | 5 | 0 | 1 |
| phaseErrorIonosphericModel(GroundStation, FieldSpacecraftState, CalculusFieldElement[]) | | 100% | | n/a | 0 | 1 | 0 | 4 | 0 | 1 |
| phaseErrorJacobianState(double[], int) | | 100% | | 100% | 0 | 2 | 0 | 4 | 0 | 1 |
| phaseErrorParameterDerivative(GroundStation, ParameterDriver, SpacecraftState) | | 100% | | n/a | 0 | 1 | 0 | 4 | 0 | 1 |
| PhaseIonosphericDelayModifier(IonosphericModel, double) | | 100% | | n/a | 0 | 1 | 0 | 4 | 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 |