Native propagation with the rounded source installed
24/24 matched native controls passed.
Charged 78 native evaluations and 348 bounds; preserved 348 directional acceleration certificates. Elapsed 201.31 seconds.
Reserved 7,536/7,536 source-reference steps and 7,536/7,536 rounded body bounds separately from full native evaluations.
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; compiled primitive arithmetic rounds outward and includes center-operation error. coordinate bounds now survive force, velocity and geographic extraction. The qualified rounded source interval is installed at each actual midpoint; later force differences and the original numerical centers are retained.
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.