rangeRateErrorTroposphericModel(GroundStation, FieldSpacecraftState, CalculusFieldElement[]) |   | 97% |   | 50% | 1 | 2 | 1 | 17 | 0 | 1 |
rangeRateErrorTroposphericModel(GroundStation, SpacecraftState) |   | 97% |   | 50% | 1 | 2 | 1 | 15 | 0 | 1 |
modify(EstimatedMeasurement) |  | 100% |  | 100% | 0 | 7 | 0 | 38 | 0 | 1 |
rangeRateErrorParameterDerivative(double[], int) |  | 100% |  | 100% | 0 | 2 | 0 | 5 | 0 | 1 |
rangeRateErrorParameterDerivative(GroundStation, ParameterDriver, SpacecraftState) |  | 100% | | n/a | 0 | 1 | 0 | 4 | 0 | 1 |
RangeRateTroposphericDelayModifier(DiscreteTroposphericModel, boolean) |  | 100% |  | 100% | 0 | 2 | 0 | 6 | 0 | 1 |
rangeRateErrorJacobianState(double[]) |  | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
getParametersDrivers() |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |