BetaAngleDetector(AdaptableInterval, double, int, EventHandler, double, PVCoordinatesProvider, Frame) | | 100% | | n/a | 0 | 1 | 0 | 5 | 0 | 1 |
withCelestialProvider(PVCoordinatesProvider) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
withBetaThreshold(double) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
withInertialFrame(Frame) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
calculateBetaAngle(SpacecraftState, PVCoordinatesProvider, Frame) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
create(AdaptableInterval, double, int, EventHandler) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
BetaAngleDetector(double, PVCoordinatesProvider, Frame) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
g(SpacecraftState) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
BetaAngleDetector(double) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
calculateBetaAngle(SpacecraftState, PVCoordinatesProvider) | | 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 |