PositionAngleDetector(AdaptableInterval, double, int, EventHandler, OrbitType, PositionAngleType, double) |  | 100% |  | 100% | 0 | 4 | 0 | 15 | 0 | 1 |
g(SpacecraftState) |  | 100% |  | 100% | 0 | 3 | 0 | 12 | 0 | 1 |
init(SpacecraftState, AbsoluteDate) |  | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
create(AdaptableInterval, double, int, EventHandler) |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
PositionAngleDetector(double, double, OrbitType, PositionAngleType, double) |  | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
PositionAngleDetector(OrbitType, PositionAngleType, double) |  | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
lambda$new$3(OrbitType, PositionAngleType, Orbit) |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
lambda$new$2(OrbitType, PositionAngleType, Orbit) |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
lambda$new$1(OrbitType, PositionAngleType, Orbit) |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getOrbitType() |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getPositionAngleType() |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getAngle() |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
lambda$new$0(double, SpacecraftState) |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |