Rotation/gain support component

24/24 controls pass; state: complete.

Checked 1536 physical probes, 119808 exact inequalities.

The necessary inequalities preserve seven source-qualified independent vector checks in the existing shared errors. All 27 physical and 24 shared-error coordinates remain. Independent Rodrigues/force oracles check the supplied mathematical construction; exact reciprocal chords and outward coefficients preserve physical matrix columns.

No native integrations, original aircraft reads, observed fits or protected ESA outcomes occur. This does not establish whole-program floating-point enclosure, aircraft uncertainty or narrower prediction ranges. A separately frozen saved-case comparison is required before applying the component.

Frozen scope · Derivation · Roadmap.

Maximum independent-oracle difference: 1.42e-15.