| rangeRateErrorTroposphericModel(GroundStation, FieldSpacecraftState, RealFieldElement[]) |   | 97% | | 50% | 1 | 2 | 1 | 18 | 0 | 1 |
| rangeRateErrorTroposphericModel(GroundStation, SpacecraftState) | | 97% | | 50% | 1 | 2 | 1 | 16 | 0 | 1 |
| modify(EstimatedMeasurement) | | 100% | | 100% | 0 | 8 | 0 | 40 | 0 | 1 |
| rangeRateErrorParameterDerivative(double[], int) | | 100% | | 100% | 0 | 2 | 0 | 5 | 0 | 1 |
| rangeRateErrorJacobianState(double[], int) | | 100% | | 100% | 0 | 2 | 0 | 4 | 0 | 1 |
| rangeRateErrorParameterDerivative(GroundStation, ParameterDriver, SpacecraftState) | | 100% | | n/a | 0 | 1 | 0 | 4 | 0 | 1 |
| rangeRateErrorJacobianState(GroundStation, SpacecraftState) | | 100% | | n/a | 0 | 1 | 0 | 4 | 0 | 1 |
| RangeRateTroposphericDelayModifier(DiscreteTroposphericModel, boolean) | | 100% | | 100% | 0 | 2 | 0 | 6 | 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 |
| getParametersDrivers() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |