Local Level Lab

Airborne measurements. Open methods.

Prediction with shared vector-norm bounds

48/48 cases pass correctness.

All six groups meet the unchanged twofold target against the projected baseline: no.

Candidate / removal Complete Width N / E / height (m) Ratio to immediate predecessor Twofold target
Globe with specified field / zero Yes 1.2710, 1.6445, 1.0732 0.9997, 0.9995, 1.0000 No
Globe with specified field / profiled Yes 1.3564, 1.7195, 1.1596 0.9997, 0.9996, 1.0000 No
Globe with zero field / zero Yes 0.9751, 1.0492, 0.7554 1.0000, 1.0000, 1.0000 Yes
Globe with zero field / profiled Yes 1.1306, 1.1951, 0.9115 0.9999, 0.9999, 1.0000 No
Flat disc / zero Yes 0.6973, 0.2194, 0.5216 1.0000, 0.9999, 1.0000 Yes
Flat disc / profiled Yes 0.8867, 0.2782, 0.7047 0.9999, 0.9999, 1.0000 Yes

Elapsed 36.9 seconds. Native calls and bounds: zero. The comparison reuses sealed generated results and adds qualified necessary vector-norm constraints. All original physical bounds and sectors remain. Future outcomes are checked only after prediction is saved. These widths are not measured aircraft errors or calibrated intervals.

Frozen scope · Component qualification · Predecessor · Roadmap.