theoreticalEvaluation(int, int, SpacecraftState[]) | | 100% | | 90% | 1 | 6 | 0 | 44 | 0 | 1 |
oneWayTheoreticalEvaluation(int, int, boolean, TimeStampedFieldPVCoordinates, TimeStampedFieldPVCoordinates, SpacecraftState, Map) | | 100% | | 100% | 0 | 5 | 0 | 18 | 0 | 1 |
BistaticRangeRate(GroundStation, GroundStation, AbsoluteDate, double, double, double, ObservableSatellite) | | 100% | | n/a | 0 | 1 | 0 | 23 | 0 | 1 |
lambda$theoreticalEvaluation$0(EstimatedMeasurement, EstimatedMeasurement, EstimatedMeasurement, ParameterDriver) | | 100% | | 100% | 0 | 2 | 0 | 7 | 0 | 1 |
getEmitterStation() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getReceiverStation() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |