modify(EstimatedMeasurement) |   | 81% |   | 66% | 3 | 7 | 7 | 38 | 0 | 1 |
rangeRateErrorParameterDerivative(double[], int) |  | 0% |  | 0% | 2 | 2 | 5 | 5 | 1 | 1 |
RangeRateIonosphericDelayModifier(IonosphericModel, double, boolean) |   | 83% |   | 50% | 1 | 2 | 1 | 7 | 0 | 1 |
rangeRateErrorIonosphericModel(GroundStation, SpacecraftState) |  | 100% | | n/a | 0 | 1 | 0 | 6 | 0 | 1 |
rangeRateErrorIonosphericModel(GroundStation, FieldSpacecraftState, RealFieldElement[]) |  | 100% | | n/a | 0 | 1 | 0 | 6 | 0 | 1 |
rangeRateErrorParameterDerivative(GroundStation, ParameterDriver, SpacecraftState) |  | 100% | | n/a | 0 | 1 | 0 | 4 | 0 | 1 |
rangeRateErrorJacobianState(double[]) |  | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
getParametersDrivers() |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |