acceleration(FieldSpacecraftState, CalculusFieldElement[]) | | 100% | | 100% | 0 | 3 | 0 | 8 | 0 | 1 |
acceleration(SpacecraftState, double[]) | | 100% | | 100% | 0 | 3 | 0 | 8 | 0 | 1 |
ParametricAcceleration(Vector3D, boolean, AttitudeProvider, AccelerationModel) | | 100% | | n/a | 0 | 1 | 0 | 6 | 0 | 1 |
ParametricAcceleration(Vector3D, boolean, AccelerationModel) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
ParametricAcceleration(Vector3D, AttitudeProvider, AccelerationModel) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
init(SpacecraftState, AbsoluteDate) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
getParametersDrivers() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
dependsOnPositionOnly() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getEventDetectors() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getFieldEventDetectors(Field) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |