calculateBetaAngle(SpacecraftState, PVCoordinatesProvider, Frame) |  | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
BetaAngleDetector(EventDetectionSettings, 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 |
g(SpacecraftState) |  | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
create(EventDetectionSettings, EventHandler) |  | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
BetaAngleDetector(double, PVCoordinatesProvider, Frame) |  | 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 |