phaseErrorTroposphericModel(GroundStation, FieldSpacecraftState, CalculusFieldElement[], double) | | 95% | | 50% | 1 | 2 | 1 | 10 | 0 | 1 |
phaseErrorTroposphericModel(GroundStation, SpacecraftState, double) | | 94% | | 50% | 1 | 2 | 1 | 8 | 0 | 1 |
modify(EstimatedMeasurement) | | 100% | | 91% | 1 | 7 | 0 | 37 | 0 | 1 |
phaseErrorParameterDerivative(double[], int) | | 100% | | 100% | 0 | 2 | 0 | 5 | 0 | 1 |
phaseErrorParameterDerivative(GroundStation, ParameterDriver, SpacecraftState, double) | | 100% | | n/a | 0 | 1 | 0 | 4 | 0 | 1 |
phaseErrorJacobianState(double[]) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
PhaseTroposphericDelayModifier(DiscreteTroposphericModel) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
lambda$phaseErrorParameterDerivative$0(GroundStation, SpacecraftState, double, ParameterDriver) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getParametersDrivers() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |