Complete 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 | 385.675, 171.760, 118.457 | 0.501, 0.292, 0.232 |
| case-0-1-400 | 8 | 0 | True | 385.680, 171.767, 118.462 | 0.501, 0.292, 0.232 |
| case-1-0-400 | 8 | 0 | True | 385.658, 171.797, 118.458 | 0.501, 0.292, 0.232 |
| case-1-1-400 | 8 | 0 | True | 385.665, 171.805, 118.464 | 0.501, 0.292, 0.232 |
| case-2-0-400 | 8 | 0 | True | 386.075, 50.706, 118.460 | 0.501, 0.292, 0.232 |
| case-2-1-400 | 8 | 0 | True | 386.082, 50.709, 118.468 | 0.501, 0.292, 0.232 |
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 192 native evaluations in 411.15 seconds. No original files, Earth-model fits or protected ESA outcomes are used.
Frozen method and allowance · Saved broad-box baseline · Roadmap.