| modify(EstimatedMeasurement) |   | 71% | | 64% | 6 | 15 | 16 | 57 | 0 | 1 |
| modifyWithoutDerivatives(EstimatedMeasurementBase) | | 0% | | n/a | 1 | 1 | 10 | 10 | 1 | 1 |
| rangeErrorParameterDerivative(double[], int) | | 0% | | n/a | 1 | 1 | 1 | 1 | 1 | 1 |
| getEffectName() | | 0% | | n/a | 1 | 1 | 1 | 1 | 1 | 1 |
| rangeErrorParameterDerivative(Observer, ParameterDriver, SpacecraftState) | | 100% | | n/a | 0 | 1 | 0 | 4 | 0 | 1 |
| rangeErrorIonosphericModel(Observer, SpacecraftState) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| rangeErrorJacobianState(double[]) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
| rangeErrorIonosphericModel(Observer, FieldSpacecraftState, CalculusFieldElement[]) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| TurnAroundRangeIonosphericDelayModifier(IonosphericModel, double) | | 100% | | n/a | 0 | 1 | 0 | 4 | 0 | 1 |
| getParametersDrivers() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |