Shared-reference orientation-cover feasibility
48/48 sector identities pass; state: complete.
Eight sectors cover the full original yaw range for each model/processing case. All other calibration directions remain. Union widths include every sector not excluded by checked necessary constraints. These are generated mathematical ranges, not measured aircraft errors.
| Case | Sectors | Excluded | Complete | Future union width N / E / height (m) | Ratio to broad-box baseline |
|---|---|---|---|---|---|
| case-0-0-400 | 8 | 0 | True | 31.626, 31.497, 31.228 | 0.041, 0.054, 0.061 |
| case-0-1-400 | 8 | 0 | True | 31.628, 31.500, 31.230 | 0.041, 0.054, 0.061 |
| case-1-0-400 | 8 | 0 | True | 31.596, 31.509, 31.178 | 0.041, 0.054, 0.061 |
| case-1-1-400 | 8 | 0 | True | 31.619, 31.532, 31.201 | 0.041, 0.054, 0.061 |
| case-2-0-400 | 8 | 0 | True | 31.597, 9.294, 31.161 | 0.041, 0.054, 0.061 |
| case-2-1-400 | 8 | 0 | True | 31.619, 9.301, 31.183 | 0.041, 0.054, 0.061 |
A tenfold reduction is a component target, not qualification of long-record observational prediction. A correct but broad result leaves dependent observed fits blocked. Global floating-point error, actual receiver covariance and full-flight adequacy remain open.
Charged 144 native evaluations in 587.98 seconds. No original files, Earth-model fits or protected ESA outcomes are used.
Frozen method and allowance · Saved broad-box baseline · Roadmap.
All 27 physical and six common-error columns remain. One common block is used across training and future epochs; original inputs, physical bounds and acceptance limits are preserved.
| Case | Ratio to regrouped widths N / E / height |
|---|---|
| case-0-0-400 | 0.274, 0.274, 0.272 |
| case-0-1-400 | 0.274, 0.274, 0.272 |
| case-1-0-400 | 0.274, 0.274, 0.272 |
| case-1-1-400 | 0.274, 0.274, 0.272 |
| case-2-0-400 | 0.274, 0.274, 0.272 |
| case-2-1-400 | 0.274, 0.274, 0.272 |