modify(EstimatedMeasurement) | | 74% | | 57% | 8 | 15 | 16 | 62 | 0 | 1 |
modifyWithoutDerivatives(EstimatedMeasurementBase) | | 0% | | n/a | 1 | 1 | 10 | 10 | 1 | 1 |
rangeErrorParameterDerivative(double[], int) | | 0% | | n/a | 1 | 1 | 1 | 1 | 1 | 1 |
rangeErrorParameterDerivative(GroundStation, ParameterDriver, SpacecraftState) | | 100% | | n/a | 0 | 1 | 0 | 4 | 0 | 1 |
rangeErrorIonosphericModel(GroundStation, SpacecraftState) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
rangeErrorJacobianState(double[]) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
rangeErrorIonosphericModel(GroundStation, FieldSpacecraftState, CalculusFieldElement[]) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
TurnAroundRangeIonosphericDelayModifier(IonosphericModel, double) | | 100% | | n/a | 0 | 1 | 0 | 4 | 0 | 1 |
getParametersDrivers() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |