| calculateBetaAngle(FieldSpacecraftState, FieldPVCoordinatesProvider, Frame) |  | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
| FieldBetaAngleDetector(Field, CalculusFieldElement, FieldPVCoordinatesProvider, Frame) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| withCelestialProvider(FieldPVCoordinatesProvider) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| withBetaThreshold(CalculusFieldElement) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| withInertialFrame(Frame) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| FieldBetaAngleDetector(FieldAdaptableInterval, CalculusFieldElement, int, FieldEventHandler, CalculusFieldElement, FieldPVCoordinatesProvider, Frame) | | 100% | | n/a | 0 | 1 | 0 | 5 | 0 | 1 |
| create(FieldAdaptableInterval, CalculusFieldElement, int, FieldEventHandler) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| g(FieldSpacecraftState) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| FieldBetaAngleDetector(CalculusFieldElement) | | 100% | | n/a | 0 | 1 | 0 | 4 | 0 | 1 |
| calculateBetaAngle(FieldSpacecraftState, FieldPVCoordinatesProvider) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getCelestialBodyProvider() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getInertialFrame() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getBetaAngleThreshold() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| lambda$new$0(FieldSpacecraftState) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |