| getCurrentWeight() |  | 0% | | 0% | 2 | 2 | 1 | 1 | 1 | 1 |
| setCurrentWeight(double[]) | | 0% | | n/a | 1 | 1 | 2 | 2 | 1 | 1 |
| getParameterDerivatives(ParameterDriver) |  | 98% | | 87% | 1 | 5 | 0 | 12 | 0 | 1 |
| EstimatedMeasurement(ObservedMeasurement, int, int, SpacecraftState[], TimeStampedPVCoordinates[]) | | 100% | | n/a | 0 | 1 | 0 | 10 | 0 | 1 |
| setStateDerivatives(int, double[][]) | | 100% | | 100% | 0 | 2 | 0 | 4 | 0 | 1 |
| getStateDerivatives(int) | | 100% | | 100% | 0 | 2 | 0 | 4 | 0 | 1 |
| getTimeOffset() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getDerivativesDrivers() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| setParameterDerivatives(ParameterDriver, double[]) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| setEstimatedValue(double[]) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| getStates() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getParticipants() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getEstimatedValue() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getDate() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getObservedValue() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| setStatus(EstimatedMeasurement.Status) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| lambda$getDerivativesDrivers$0(Map.Entry) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getObservedMeasurement() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getIteration() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getCount() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getStatus() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |