Regrouped 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 | 115.382, 114.979, 114.670 | 0.150, 0.195, 0.224 |
| case-0-1-400 | 8 | 0 | True | 115.387, 114.985, 114.676 | 0.150, 0.195, 0.224 |
| case-1-0-400 | 8 | 0 | True | 115.383, 115.012, 114.654 | 0.150, 0.195, 0.224 |
| case-1-1-400 | 8 | 0 | True | 115.390, 115.020, 114.660 | 0.150, 0.195, 0.224 |
| case-2-0-400 | 8 | 0 | True | 115.491, 33.945, 114.649 | 0.150, 0.195, 0.224 |
| case-2-1-400 | 8 | 0 | True | 115.499, 33.948, 114.656 | 0.150, 0.195, 0.224 |
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 471.98 seconds. No original files, Earth-model fits or protected ESA outcomes are used.
Frozen method and allowance · Saved broad-box baseline · Roadmap.
| Case | Ratio to previous orientation-cover widths N / E / height |
|---|---|
| case-0-0-400 | 0.299, 0.669, 0.968 |
| case-0-1-400 | 0.299, 0.669, 0.968 |
| case-1-0-400 | 0.299, 0.669, 0.968 |
| case-1-1-400 | 0.299, 0.669, 0.968 |
| case-2-0-400 | 0.299, 0.669, 0.968 |
| case-2-1-400 | 0.299, 0.669, 0.968 |
All original sectors, inputs and physical bounds are retained. Native outputs, full Jacobians and training/future support inputs are saved for diagnosis without new evaluations.