Local Level Lab

Airborne measurements. Open methods.

Directional acceleration in native propagation

24/24 matched native controls passed.

Charged 78 native evaluations and 348 bounds; preserved 348 directional acceleration certificates. Elapsed 79.11 seconds.

The control matrix retains the original center, stationary-pose, derivative and nonlinear-containment criteria for all three candidates and both processing assumptions. Every physical and shared-error column remains. The original acceleration remainder and shared-error caps are preserved; only the acceleration-change range comes from the new directional proof.

These controls qualify the native component on generated inputs. They do not establish useful full-recording prediction ranges, floating-execution enclosure or calibrated observation-error coverage. No aircraft observation was fitted, and no protected ESA data was used.

Frozen scope · Static force controls · Roadmap.