rangeRateErrorTroposphericModel(GroundStation, FieldSpacecraftState, RealFieldElement[]) | | 97% | | 50% | 1 | 2 | 1 | 18 | 0 | 1 |
rangeRateErrorTroposphericModel(GroundStation, SpacecraftState) | | 97% | | 50% | 1 | 2 | 1 | 16 | 0 | 1 |
modify(EstimatedMeasurement) | | 100% | | 100% | 0 | 8 | 0 | 40 | 0 | 1 |
rangeRateErrorParameterDerivative(double[], int) | | 100% | | 100% | 0 | 2 | 0 | 5 | 0 | 1 |
rangeRateErrorJacobianState(double[], int) | | 100% | | 100% | 0 | 2 | 0 | 4 | 0 | 1 |
rangeRateErrorParameterDerivative(GroundStation, ParameterDriver, SpacecraftState) | | 100% | | n/a | 0 | 1 | 0 | 4 | 0 | 1 |
rangeRateErrorJacobianState(GroundStation, SpacecraftState) | | 100% | | n/a | 0 | 1 | 0 | 4 | 0 | 1 |
RangeRateTroposphericDelayModifier(DiscreteTroposphericModel, boolean) | | 100% | | 100% | 0 | 2 | 0 | 6 | 0 | 1 |
getStationHeightAMSL(Field, GroundStation) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
getStationHeightAMSL(GroundStation) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
getParametersDrivers() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |