modify(EstimatedMeasurement) | | 76% | | 68% | 5 | 12 | 16 | 63 | 0 | 1 |
rangeErrorParameterDerivative(double[], int) | | 0% | | 0% | 2 | 2 | 5 | 5 | 1 | 1 |
rangeErrorJacobianState(double[], int) | | 0% | | 0% | 2 | 2 | 4 | 4 | 1 | 1 |
rangeErrorTroposphericModel(GroundStation, FieldSpacecraftState, RealFieldElement[]) | | 95% | | 50% | 1 | 2 | 1 | 11 | 0 | 1 |
rangeErrorTroposphericModel(GroundStation, SpacecraftState) | | 94% | | 50% | 1 | 2 | 1 | 9 | 0 | 1 |
rangeErrorParameterDerivative(GroundStation, ParameterDriver, SpacecraftState) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
rangeErrorJacobianState(GroundStation, SpacecraftState) | | 100% | | n/a | 0 | 1 | 0 | 4 | 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 |
TurnAroundRangeTroposphericDelayModifier(DiscreteTroposphericModel) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
getParametersDrivers() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |