dependsOnPositionOnly() | | 100% | | 66% | 2 | 4 | 0 | 1 | 0 | 1 |
acceleration(SpacecraftState, double[]) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
acceleration(FieldSpacecraftState, CalculusFieldElement[]) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
getFieldEventDetectors(Field) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
init(SpacecraftState, AbsoluteDate) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
init(FieldSpacecraftState, FieldAbsoluteDate) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
getEventDetectors() | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
RadiationPressureModel(LightFluxModel, RadiationSensitive) | | 100% | | n/a | 0 | 1 | 0 | 4 | 0 | 1 |
getParametersDrivers() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getRadiationSensitive() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getLightFluxModel() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |