| modify(EstimatedMeasurement) |   | 76% | | 68% | 5 | 12 | 16 | 63 | 0 | 1 |
| rangeErrorParameterDerivative(double[], int) | | 0% | | 0% | 2 | 2 | 5 | 5 | 1 | 1 |
| rangeErrorJacobianState(double[], int) | | 0% | | 0% | 2 | 2 | 4 | 4 | 1 | 1 |
| rangeErrorTroposphericModel(GroundStation, FieldSpacecraftState, RealFieldElement[]) | | 95% | | 50% | 1 | 2 | 1 | 11 | 0 | 1 |
| rangeErrorTroposphericModel(GroundStation, SpacecraftState) | | 94% | | 50% | 1 | 2 | 1 | 9 | 0 | 1 |
| rangeErrorParameterDerivative(GroundStation, ParameterDriver, SpacecraftState) | | 100% | | n/a | 0 | 1 | 0 | 3 | 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 |
| TurnAroundRangeTroposphericDelayModifier(DiscreteTroposphericModel) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
| getParametersDrivers() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |