getParameterDerivatives(ParameterDriver) | | 79% | | 80% | 2 | 6 | 1 | 13 | 0 | 1 |
setParameterDerivatives(ParameterDriver, AbsoluteDate, double[]) | | 87% | | 75% | 2 | 5 | 1 | 13 | 0 | 1 |
getParameterDerivatives(ParameterDriver, AbsoluteDate) | | 98% | | 87% | 1 | 5 | 0 | 11 | 0 | 1 |
setStateDerivatives(int, double[][]) | | 100% | | 100% | 0 | 2 | 0 | 4 | 0 | 1 |
getStateDerivatives(int) | | 100% | | 100% | 0 | 2 | 0 | 4 | 0 | 1 |
EstimatedMeasurement(ObservedMeasurement, int, int, SpacecraftState[], TimeStampedPVCoordinates[]) | | 100% | | n/a | 0 | 1 | 0 | 4 | 0 | 1 |
getStateSize() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getDerivativesDrivers() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
setParameterDerivatives(ParameterDriver, TimeSpanMap) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
lambda$getDerivativesDrivers$0(Map.Entry) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |