g(FieldSpacecraftState) | | 53% | | 50% | 2 | 3 | 3 | 10 | 0 | 1 |
create(FieldEventDetectionSettings, FieldEventHandler) | | 0% | | n/a | 1 | 1 | 1 | 1 | 1 | 1 |
withElevationMask(ElevationMask) | | 0% | | n/a | 1 | 1 | 1 | 1 | 1 | 1 |
getElevationMask() | | 0% | | n/a | 1 | 1 | 1 | 1 | 1 | 1 |
FieldElevationDetector(CalculusFieldElement, CalculusFieldElement, TopocentricFrame) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
FieldElevationDetector(FieldEventDetectionSettings, FieldEventHandler, double, ElevationMask, AtmosphericRefractionModel, TopocentricFrame) | | 100% | | n/a | 0 | 1 | 0 | 6 | 0 | 1 |
FieldElevationDetector(Field, TopocentricFrame) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
withRefraction(AtmosphericRefractionModel) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
withConstantElevation(double) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getMinElevation() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getRefractionModel() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getTopocentricFrame() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |