| modify(EstimatedMeasurement) |   | 81% | | 75% | 3 | 9 | 4 | 33 | 0 | 1 |
| phaseErrorParameterDerivative(Observer, ParameterDriver, SpacecraftState, double) | | 0% | | n/a | 1 | 1 | 4 | 4 | 1 | 1 |
| phaseErrorTroposphericModel(Observer, FieldSpacecraftState, CalculusFieldElement[], double) | | 82% | | 50% | 2 | 3 | 2 | 11 | 0 | 1 |
| phaseErrorTroposphericModel(Observer, SpacecraftState, double) | | 80% | | 50% | 2 | 3 | 2 | 9 | 0 | 1 |
| lambda$phaseErrorParameterDerivative$0(Observer, SpacecraftState, double, ParameterDriver, AbsoluteDate) | | 0% | | n/a | 1 | 1 | 1 | 1 | 1 | 1 |
| getEffectName() | | 0% | | n/a | 1 | 1 | 1 | 1 | 1 | 1 |
| modifyWithoutDerivatives(EstimatedMeasurementBase) | | 100% | | n/a | 0 | 1 | 0 | 8 | 0 | 1 |
| phaseErrorJacobianState(double[]) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
| PhaseTroposphericDelayModifier(TroposphericModel) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
| phaseErrorParameterDerivative(double[], int) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getParametersDrivers() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |