| dragAcceleration(AbsoluteDate, Frame, Vector3D, Rotation, double, double, Vector3D, String) |  | 0% | | n/a | 1 | 1 | 1 | 1 | 1 | 1 |
| dragAcceleration(AbsoluteDate, Frame, FieldVector3D, FieldRotation, DerivativeStructure, DerivativeStructure, FieldVector3D) | | 0% | | n/a | 1 | 1 | 1 | 1 | 1 | 1 |
| radiationPressureAcceleration(AbsoluteDate, Frame, Vector3D, Rotation, double, Vector3D, String) | | 0% | | n/a | 1 | 1 | 1 | 1 | 1 | 1 |
| radiationPressureAcceleration(AbsoluteDate, Frame, FieldVector3D, FieldRotation, DerivativeStructure, FieldVector3D) | | 0% | | n/a | 1 | 1 | 1 | 1 | 1 | 1 |
| setDragCoefficient(double) | | 0% | | n/a | 1 | 1 | 2 | 2 | 1 | 1 |
| setAbsorptionCoefficient(double) | | 0% | | n/a | 1 | 1 | 2 | 2 | 1 | 1 |
| setReflectionCoefficient(double) | | 0% | | n/a | 1 | 1 | 2 | 2 | 1 | 1 |
| getDragCoefficient() | | 0% | | n/a | 1 | 1 | 1 | 1 | 1 | 1 |
| getAbsorptionCoefficient() | | 0% | | n/a | 1 | 1 | 1 | 1 | 1 | 1 |
| getReflectionCoefficient() | | 0% | | n/a | 1 | 1 | 1 | 1 | 1 | 1 |
| SphericalSpacecraft(double, double, double, double) |  | 100% | | n/a | 0 | 1 | 0 | 4 | 0 | 1 |
| dragAcceleration(AbsoluteDate, Frame, Vector3D, Rotation, double, double, Vector3D) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| radiationPressureAcceleration(AbsoluteDate, Frame, Vector3D, Rotation, double, Vector3D) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |