Common-acceleration 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 | 0.277, 0.350, 0.194 | 0.000, 0.001, 0.000 |
| case-0-1-400 | 8 | 0 | True | 0.286, 0.358, 0.202 | 0.000, 0.001, 0.000 |
| case-1-0-400 | 8 | 0 | True | 0.225, 0.236, 0.138 | 0.000, 0.000, 0.000 |
| case-1-1-400 | 8 | 0 | True | 0.243, 0.253, 0.156 | 0.000, 0.000, 0.000 |
| case-2-0-400 | 8 | 0 | True | 0.183, 0.061, 0.123 | 0.000, 0.000, 0.000 |
| case-2-1-400 | 8 | 0 | True | 0.205, 0.068, 0.145 | 0.000, 0.000, 0.000 |
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 1432.63 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 15 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 previous shared-reference widths N / E / height |
|---|---|
| case-0-0-400 | 0.009, 0.011, 0.006 |
| case-0-1-400 | 0.009, 0.011, 0.006 |
| case-1-0-400 | 0.007, 0.007, 0.004 |
| case-1-1-400 | 0.008, 0.008, 0.005 |
| case-2-0-400 | 0.006, 0.007, 0.004 |
| case-2-1-400 | 0.006, 0.007, 0.005 |