| modify(EstimatedMeasurement) |   | 81% | | 66% | 3 | 7 | 7 | 38 | 0 | 1 |
| rangeRateErrorParameterDerivative(double[], int) | | 0% | | 0% | 2 | 2 | 5 | 5 | 1 | 1 |
| RangeRateIonosphericDelayModifier(IonosphericModel, double, boolean) | | 83% | | 50% | 1 | 2 | 1 | 7 | 0 | 1 |
| rangeRateErrorIonosphericModel(GroundStation, SpacecraftState) | | 100% | | n/a | 0 | 1 | 0 | 6 | 0 | 1 |
| rangeRateErrorIonosphericModel(GroundStation, FieldSpacecraftState, CalculusFieldElement[]) | | 100% | | n/a | 0 | 1 | 0 | 6 | 0 | 1 |
| rangeRateErrorParameterDerivative(GroundStation, ParameterDriver, SpacecraftState) | | 100% | | n/a | 0 | 1 | 0 | 4 | 0 | 1 |
| rangeRateErrorJacobianState(double[]) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
| getParametersDrivers() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |