RangeRate(GroundStation, AbsoluteDate, double, double, double, boolean) | | 0% | | n/a | 1 | 1 | 2 | 2 | 1 | 1 |
RangeRate(GroundStation, AbsoluteDate, double, double, double, boolean, int) | | 0% | | n/a | 1 | 1 | 2 | 2 | 1 | 1 |
theoreticalEvaluation(int, int, SpacecraftState[]) | | 100% | | 100% | 0 | 6 | 0 | 55 | 0 | 1 |
oneWayTheoreticalEvaluation(int, int, boolean, TimeStampedFieldPVCoordinates, TimeStampedFieldPVCoordinates, SpacecraftState, Map) | | 100% | | 100% | 0 | 5 | 0 | 18 | 0 | 1 |
RangeRate(GroundStation, AbsoluteDate, double, double, double, boolean, ObservableSatellite) | | 100% | | n/a | 0 | 1 | 0 | 14 | 0 | 1 |
lambda$theoreticalEvaluation$0(EstimatedMeasurement, EstimatedMeasurement, EstimatedMeasurement, ParameterDriver) | | 100% | | 100% | 0 | 2 | 0 | 7 | 0 | 1 |
isTwoWay() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getStation() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |