Native propagation with direct source remainders
24/24 matched native controls passed.
Charged 78 native evaluations and 348 bounds; preserved 348 directional acceleration certificates. Elapsed 232.83 seconds.
Reserved 7,536/7,536 source-reference steps and 7,536/7,536 rounded body bounds separately from full native evaluations.
Every successful bound preserves the sealed predecessor prediction, three coefficient matrices, physical bindings exactly, without widening any of the four remainder arrays. 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.