| modify(EstimatedMeasurement) |   | 78% | | 60% | 6 | 11 | 14 | 59 | 0 | 1 |
| rangeErrorParameterDerivative(double[], int) | | 0% | | 0% | 2 | 2 | 5 | 5 | 1 | 1 |
| rangeErrorParameterDerivative(GroundStation, ParameterDriver, SpacecraftState) | | 100% | | n/a | 0 | 1 | 0 | 4 | 0 | 1 |
| rangeErrorIonosphericModel(GroundStation, SpacecraftState) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
| rangeErrorIonosphericModel(GroundStation, FieldSpacecraftState, CalculusFieldElement[]) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
| rangeErrorJacobianState(double[]) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
| TurnAroundRangeIonosphericDelayModifier(IonosphericModel, double) | | 100% | | n/a | 0 | 1 | 0 | 4 | 0 | 1 |
| getParametersDrivers() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |