calculateBetaAngle(FieldSpacecraftState, FieldPVCoordinatesProvider, Frame) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
FieldBetaAngleDetector(FieldAdaptableInterval, CalculusFieldElement, int, FieldEventHandler, CalculusFieldElement, FieldPVCoordinatesProvider, Frame) | | 100% | | n/a | 0 | 1 | 0 | 5 | 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 |
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 |