| modify(EstimatedMeasurement) |   | 71% | | 64% | 6 | 15 | 18 | 60 | 0 | 1 |
| rangeErrorTroposphericModel(Observer, FieldSpacecraftState, CalculusFieldElement[]) | | 80% | | 50% | 2 | 3 | 2 | 10 | 0 | 1 |
| rangeErrorTroposphericModel(Observer, SpacecraftState) | | 78% | | 50% | 2 | 3 | 2 | 8 | 0 | 1 |
| rangeErrorParameterDerivative(double[], int) | | 0% | | n/a | 1 | 1 | 1 | 1 | 1 | 1 |
| getEffectName() | | 0% | | n/a | 1 | 1 | 1 | 1 | 1 | 1 |
| modifyWithoutDerivatives(EstimatedMeasurementBase) | | 100% | | n/a | 0 | 1 | 0 | 10 | 0 | 1 |
| rangeErrorParameterDerivative(Observer, ParameterDriver, SpacecraftState) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
| rangeErrorJacobianState(double[]) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
| TurnAroundRangeTroposphericDelayModifier(TroposphericModel) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
| lambda$rangeErrorParameterDerivative$0(Observer, SpacecraftState, ParameterDriver, AbsoluteDate) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getParametersDrivers() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |