radiationPressureAcceleration(AbsoluteDate, Frame, Vector3D, Rotation, double, Vector3D, String) | | 82% | | 75% | 1 | 3 | 1 | 9 | 0 | 1 |
dragAcceleration(AbsoluteDate, Frame, Vector3D, Rotation, double, double, Vector3D, String) | | 67% | | 50% | 1 | 2 | 1 | 4 | 0 | 1 |
radiationPressureAcceleration(AbsoluteDate, Frame, FieldVector3D, FieldRotation, DerivativeStructure, FieldVector3D) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
radiationPressureAcceleration(AbsoluteDate, Frame, Vector3D, Rotation, double, Vector3D) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
dragAcceleration(AbsoluteDate, Frame, FieldVector3D, FieldRotation, DerivativeStructure, double, FieldVector3D) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
dragAcceleration(AbsoluteDate, Frame, Vector3D, Rotation, double, double, Vector3D) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
SphericalSpacecraft(double, double, double, double) | | 100% | | n/a | 0 | 1 | 0 | 6 | 0 | 1 |
setDragCoefficient(double) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
setAbsorptionCoefficient(double) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
setReflectionCoefficient(double) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
getDragCoefficient() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getAbsorptionCoefficient() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getReflectionCoefficient() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |