| phaseErrorTroposphericModel(GroundStation, FieldSpacecraftState, RealFieldElement[], double) |   | 95% | | 50% | 1 | 2 | 1 | 11 | 0 | 1 |
| phaseErrorTroposphericModel(GroundStation, SpacecraftState, double) | | 94% | | 50% | 1 | 2 | 1 | 9 | 0 | 1 |
| modify(EstimatedMeasurement) | | 100% | | 91% | 1 | 7 | 0 | 37 | 0 | 1 |
| phaseErrorParameterDerivative(double[], int) | | 100% | | 100% | 0 | 2 | 0 | 5 | 0 | 1 |
| phaseErrorParameterDerivative(GroundStation, ParameterDriver, SpacecraftState, double) | | 100% | | n/a | 0 | 1 | 0 | 4 | 0 | 1 |
| phaseErrorJacobianState(double[]) | | 100% | | n/a | 0 | 1 | 0 | 3 | 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 |
| PhaseTroposphericDelayModifier(DiscreteTroposphericModel) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
| lambda$phaseErrorParameterDerivative$0(GroundStation, SpacecraftState, double, ParameterDriver) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getParametersDrivers() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |