Common force-transform component controls

24/24 controls pass; state: complete.

Checked 1536 probes, 1296 independent derivative evaluations and 6144 weighted-map identities.

Independent Rodrigues and reciprocal-gain calculations check the matrix. All 27 physical columns and nine new common-error coordinates remain, alongside the previous 15 shared coordinates: 51 columns in total. The synthetic near-boundary gain control tests mathematics and changes no aircraft calibration limit.

This qualifies the common matrix component only. Integrated clock dependence, native propagation, a typed joint prediction interface, full-range usefulness and observational coverage remain unqualified. No native integration, original aircraft reads or observed fits occur.

Frozen component scope · Derivation and next gates · Roadmap.

Maximum independent matrix error: 2.31e-14; derivative error: 4.57e-11; weighted-map error: 9.09e-13.