| rangeErrorTroposphericModel(GroundStation, FieldSpacecraftState, CalculusFieldElement[]) |   | 95% | | 50% | 1 | 2 | 1 | 10 | 0 | 1 |
| rangeErrorTroposphericModel(GroundStation, SpacecraftState) | | 94% | | 50% | 1 | 2 | 1 | 8 | 0 | 1 |
| modify(EstimatedMeasurement) | | 100% | | 100% | 0 | 7 | 0 | 38 | 0 | 1 |
| rangeErrorParameterDerivative(double[], int) | | 100% | | 100% | 0 | 2 | 0 | 5 | 0 | 1 |
| rangeErrorParameterDerivative(GroundStation, ParameterDriver, SpacecraftState) | | 100% | | n/a | 0 | 1 | 0 | 4 | 0 | 1 |
| rangeErrorJacobianState(double[]) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
| RangeTroposphericDelayModifier(DiscreteTroposphericModel) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
| getParametersDrivers() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |