test_spacecraftHubOnlyFastPath
Unit tests for the automatic hub-only spacecraft dynamics fast path.
When no state effectors are attached and point \(B\) is colocated with the
hub center of mass, Spacecraft can bypass the general Backsubstitution
matrix assembly and ask HubEffector to compute direct rigid-body
derivatives. This test validates the resulting translational and rotational
dynamics against a simple analytic case.