Direct source-remainder component controls
13/13 fixed controls passed.
Charged 18/18 bound calls and 8/8 rotation-argument steps. Elapsed 3.64 seconds.
These controls exercise exact calibration, clipped-clock remainders, shared-parameter products and noncommuting rotation prefixes, including nonlinear arguments about nonzero references. Independent rational rotation references provide the comparison. This does not qualify the numerical-reference bridge, native source installation, complete prediction widths or observational confidence. No aircraft data, LP or fit was used.