mapOrbitToArray(FieldOrbit, PositionAngleType, CalculusFieldElement[], CalculusFieldElement[]) |   | 47% |   | 25% | 2 | 3 | 8 | 17 | 0 | 1 |
getDrivers(double, Orbit, PositionAngleType) |  | 100% |  | 100% | 0 | 3 | 0 | 12 | 0 | 1 |
normalize(Orbit, Orbit) |  | 100% |  | 100% | 0 | 2 | 0 | 27 | 0 | 1 |
normalize(FieldOrbit, FieldOrbit) |  | 100% |  | 100% | 0 | 2 | 0 | 27 | 0 | 1 |
mapOrbitToArray(Orbit, PositionAngleType, double[], double[]) |  | 100% |  | 100% | 0 | 3 | 0 | 17 | 0 | 1 |
mapArrayToOrbit(double[], double[], PositionAngleType, AbsoluteDate, double, Frame) |  | 100% |  | 100% | 0 | 2 | 0 | 3 | 0 | 1 |
mapArrayToOrbit(CalculusFieldElement[], CalculusFieldElement[], PositionAngleType, FieldAbsoluteDate, CalculusFieldElement, Frame) |  | 100% |  | 100% | 0 | 2 | 0 | 3 | 0 | 1 |
convertType(Orbit) |  | 100% |  | 100% | 0 | 2 | 0 | 1 | 0 | 1 |
convertType(FieldOrbit) |  | 100% |  | 100% | 0 | 2 | 0 | 1 | 0 | 1 |
convertToFieldOrbit(Field, Orbit) |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
{...} |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
isPositionAngleBased() |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |