Local Level Lab

Airborne measurements. Open methods.

Scalar calibration projection controls

Question

How much of a constructed acceleration-magnitude difference lies outside the local seven-parameter calibration tangent, and does the suggested linear correction actually reproduce that improvement nonlinearly within the bounds?

This is a software diagnostic, not an observed fit or nonlinear identifiability test. Neither a small nor a large projected residual establishes scientific model discrimination.

Fixed matrix and allowances

Use the independent Cartesian reference's stationary, eastbound, changing-direction and climbing profiles, three truth models, all three comparison candidates, and both reference body-orientation histories. Use 121 epochs from 0 to 600 seconds at five-second spacing. These are constructed controls, not selected aircraft trajectories or an assumed flight population.

The matrix has 72 identities, each with 121 independent-reference evaluations, 121 candidate-force evaluations and one local calibration analysis: at most 8,712 reference evaluations, 8,712 candidate-force evaluations and 72 SVDs. No optimizer starts, native integrations, original-file reads or retries. One worker, four total numerical threads, 60-second wall-time ceiling.

Apply the same calibration bounds to every candidate: three gains ±0.15, three acceleration offsets ±0.25 m/s², gravity adjustment ±0.05 m/s². These are existing assumed search bounds, not measured sensor errors. Keep all seven columns and the complete singular spectrum. Use relative rank tolerance 10⁻¹⁰.

Checks fixed before execution

Freeze task identities, sources, environment and limits before launch. Charge each identity before evaluation and preserve failures. Completed work cannot restart or transfer unused allowance. Publication verifies saved hashes and performs no numerical analysis.

The earlier frozen studies, main 53-stretch results and unresolved horizontal-only sensitivity result are unchanged. Recorded-data use remains downstream of nonlinear calibration ambiguity, timing, quantization and uncertainty controls.