| rangeErrorTroposphericModel(GroundStation, FieldSpacecraftState, RealFieldElement[]) |   | 95% | | 50% | 1 | 2 | 1 | 11 | 0 | 1 |
| rangeErrorTroposphericModel(GroundStation, SpacecraftState) | | 94% | | 50% | 1 | 2 | 1 | 9 | 0 | 1 |
| modify(EstimatedMeasurement) | | 100% | | 92% | 1 | 8 | 0 | 40 | 0 | 1 |
| rangeErrorParameterDerivative(double[], int) | | 100% | | 100% | 0 | 2 | 0 | 5 | 0 | 1 |
| rangeErrorJacobianState(double[], int) | | 100% | | 100% | 0 | 2 | 0 | 4 | 0 | 1 |
| rangeErrorParameterDerivative(GroundStation, ParameterDriver, SpacecraftState) | | 100% | | n/a | 0 | 1 | 0 | 4 | 0 | 1 |
| rangeErrorJacobianState(GroundStation, SpacecraftState) | | 100% | | n/a | 0 | 1 | 0 | 4 | 0 | 1 |
| getStationHeightAMSL(Field, GroundStation) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| getStationHeightAMSL(GroundStation) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| RangeTroposphericDelayModifier(DiscreteTroposphericModel) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
| getParametersDrivers() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |