Local Level Lab

Airborne measurements. Open methods.

Boundary-aware nonlinear controls

This completed software matrix uses ten known-answer controls, four fixed starts and three numerical strategies. It reads no NASA recordings and changes no archival results.

Strategy Fresh stopping checks Known-answer qualification Actual evaluations
rectangular 35/40 35/40 332
snapped_rectangular 38/40 38/40 346
boundary_bvls 40/40 40/40 218

Qualification checks both the existing fresh stopping tests and recovery of the known objective and predicted observations. Unique well-conditioned cases also check the parameters. A solver stopping successfully is insufficient by itself.

Control Original Snapped start Bounded linear steps
interior 4/4 4/4 4/4
boundary 3/4 4/4 4/4
redundant 3/4 4/4 4/4
scaled 4/4 4/4 4/4
nonlinear 4/4 4/4 4/4
gain_offset 4/4 4/4 4/4
curved_boundary 3/4 4/4 4/4
exponential 4/4 4/4 4/4
curved_redundant 3/4 4/4 4/4
nonlinear27 3/4 2/4 4/4

The matrix used 896 actual evaluations, within its 24,000-call ceiling. Every run retained its own 200-call limit, including fresh final checks. No failure or poor start was retried.

The new candidate passes this software matrix. Its bounded linear steps are checked against the actual nonlinear cost; rejected steps are shortened. Only boundary slack of at most one trillionth in normalized coordinates is snapped. Physical parameter limits and stopping thresholds are unchanged.

These are controls with exact derivatives and known answers, not qualification on the much larger archival observation model. They establish neither statistical significance nor recovery of any of the 41 unresolved stretches. A separate finite observed trial would be needed before rollout.

The saved results, per-run table and receipt preserve parameters, costs, stationarity, fresh checks, evaluation counts, source hashes and the numerical environment. The fixed plan defines the comparison. Default report regeneration reads the saved results only; it performs no optimization.