Local Level Lab

Airborne measurements. Open methods.

All source domains are supported

All 48 declared regions pass. Each safely inherits its parent's training constraints and acceleration bounds, and each passes the initial-source nonlinear-cap check. No calibration cap or error allowance was enlarged.

The study verified 288 parent support certificates and performed 48 source-cap calculations in 17.48 seconds with four single-thread workers. There were no trajectory predictions, optimizer starts or aircraft-data reads.

The remaining setup gate is a complete known-answer training/prediction check of the joint adapter. After that, a separately frozen comparison can test the full prediction ranges across all models, processing cases and mounting regions. The complete width target remains four of six groups; the aircraft findings remain unchanged.

Results · Frozen scope · Next-method requirements · Roadmap.