Calibration-consistency component

24/24 controls pass; state: complete.

Checked 1536 physical probes, 9216 exact inequalities and 4608 matrix-column bounds.

The six necessary constraints keep acceleration and force-matrix errors consistent with one calibration. All 27 physical and 24 shared-error coordinates remain. Independent Rodrigues/force oracles check the supplied mathematical construction; rational polynomial tails and outward row export account for the stated bounds.

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: 2.84e-14.