Local Level Lab

Airborne measurements. Open methods.

Prediction with consistent calibration errors

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 1.2714, 1.6453, 1.0732 0.9988, 0.9978, 0.9973 No
Globe with specified field / profiled Yes 1.3568, 1.7201, 1.1596 0.9988, 0.9979, 0.9975 No
Globe with zero field / zero Yes 0.9752, 1.0492, 0.7555 0.9969, 0.9958, 0.9961 Yes
Globe with zero field / profiled Yes 1.1307, 1.1952, 0.9115 0.9967, 0.9964, 0.9968 No
Flat disc / zero Yes 0.6973, 0.2194, 0.5216 0.9955, 0.9963, 0.9930 Yes
Flat disc / profiled Yes 0.8869, 0.2782, 0.7047 0.9971, 0.9969, 0.9954 Yes

Elapsed 7.9 seconds. Native calls and bounds: zero. The comparison reuses sealed generated results and adds qualified necessary calibration 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.