NASA × UDI
LIVE THESIS MODEL
Research atlas ↗

DIRECTIONALITY · RESONANCE · MEMORY · REFUSAL

UDI Live Lab.

Stress the relational interface. Change what the system can observe, break phase organization, reverse a learned direction, remove a spire, and see whether Candidate-0003 earns a commitment—or refuses.

LOAD A TEST
12 RELATIONAL MEMBERS / THREE-AXIS READOUTCOMMIT
GLOBAL COHERENCE0.896
DIRECTION ALIGNMENT0.984
SUPPORT0.671
HEADING ERROR0.0°

Explanatory reduced model. The live values interpolate relationships found in the thesis; they do not rerun the original research code or predict NASA hardware.

READ THE RESULT

The evidence supports action.

DIRECTION

Local orientation survives the interface, so the frozen core can distinguish which way a discrepancy points.

RESONANCE

The phase relationship is organized and the distributed state can compress coherently.

MEMORY

Negative and neutral consequences can reduce support for an obsolete action, although the thesis did not establish universal superiority.

NASA ANALOG

Nominal conditions are only the baseline. NASA value begins when the body, environment, or evidence changes.

THESIS LANDMARKS

Data behind the controls.

Every number below is bounded to its declared simulation. The lab uses them as landmarks, not as universal constants.

OBSERVABILITY56.7 → 96.7%

Recovery after adding locally derived orientation-sensitive relations while keeping the frozen core unchanged.

CROWN SEAT0.98415

Candidate-0003 pressure-direction alignment; rank-3 gain, condition number 1.626, and rotation error near numerical precision.

CONTINUOUS CROWN0.89588

Mean global coherence across 360 hidden runs; all 15 gates passed in the declared simulation topology.

DIRECTED MEMORY+36.53%

Matched-arrow target response over its inverse. Direction was learned, but autonomous reversal hardened and failed.

TERNARY LEDGER−39.13%

Mean active pressure versus positive-only evidence. The overall gate still failed because passive damping did better.

NEGATIVE CONTROL0% · 928

Coherent maintenance was zero in the 928-run transport-replacement matrix: extra phase data destroyed closure when it replaced geometry.

PROPOSED NASA EXPERIMENT

Move from explanatory lab to hardware falsification.

  1. 01

    Freeze the interface, baselines, protected envelope, and refusal threshold before testing.

  2. 02

    Remove a real wheel, joint, sensor, or support relation without announcing its identity.

  3. 03

    Reverse a previously useful direction and measure adaptation without erasing history.

  4. 04

    Compare fixed control, state-of-practice adaptation, UDI, and UDI-without-refusal.

  5. 05

    Report mission value retained, unsafe commitments, calibrated refusals, and recovery time.