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 back-substitution
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.