rangeErrorTroposphericModel(GroundStation, FieldSpacecraftState, RealFieldElement[]) |   | 95% |   | 50% | 1 | 2 | 1 | 11 | 0 | 1 |
rangeErrorTroposphericModel(GroundStation, SpacecraftState) |   | 94% |   | 50% | 1 | 2 | 1 | 9 | 0 | 1 |
modify(EstimatedMeasurement) |  | 100% |   | 91% | 1 | 7 | 0 | 37 | 0 | 1 |
rangeErrorParameterDerivative(double[], int) |  | 100% |  | 100% | 0 | 2 | 0 | 5 | 0 | 1 |
rangeErrorJacobianState(double[], int) |  | 100% |  | 100% | 0 | 2 | 0 | 4 | 0 | 1 |
rangeErrorParameterDerivative(GroundStation, ParameterDriver, 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 |
RangeTroposphericDelayModifier(DiscreteTroposphericModel) |  | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
getParametersDrivers() |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |