Local Level Lab

Airborne measurements. Open methods.

Common-clock force integration controls

24/24 controls pass; state: complete.

Checked 288 probes, 1296 derivative evaluations and 1728 exact rational G/H inequalities.

An independent backward suffix-weight quadrature checks the exact common-clock centres. Independent rotation/gain calculations check the matrix-weighted output. The same clock drives every packet; tag defects, matrix/clock cross terms and coefficient-export rounding remain explicit. All 27 physical columns and the 51-column augmented design remain.

This is component qualification, not native midpoint propagation, full floating-point execution certification, recording-scale usefulness or observational coverage. No native integration calls, original aircraft reads or observed fits occur.

Maximum finite-step derivative error: 3.85115e-11. Independent history queries: 270. Combined integral/oracle packet visits: 219840.

Frozen scope · Clock derivation · Native requirements · Roadmap.