⚡ OMNI-PASM v3.0: CTC_DEFLECT COMMAND CENTER

[ RETROCAUSAL INTERVENTION | QUANTUM AMPLIFICATION | NOVIKOV CONSISTENCY VERIFICATION ]
☄️
CRITICAL THREAT DETECTED: ASTEROID IMPACT
Severity
0.82
Impact Probability
76.3%
Time to Impact
T+18h
Entropy (Uncertainty)
0.237

1
THREAT DETECTION & SCAN

Multiverse Branches Scanned 8 / 8
Impact Branches Identified 3 (W0, W2, W5)
SCAN r_multiverse, target="asteroid_impact", threshold=0.70, horizon=48h → result: threat_branches = [W0, W2, W5] → average_severity = 0.82 → time_to_impact = [T+18h, T+22h, T+19h]

2
QUANTUM INTERFERENCE AMPLIFICATION

Identifying safe branches and amplifying their quantum amplitude...

Safe Branches (entropy < 0.20):
Impact Branches (entropy > 0.23):
FILTER r_multiverse, property="no_impact", entropy_max=0.20 INTERFERE r_safe_branches, mode="constructive", boost=2.5 INTERFERE r_impact_branches, mode="destructive", phase_shift=π NORMALIZE r_multiverse → Safe branch probability: 80% → Impact branch probability: 20%
Quantum Amplification Energy 2.65e-13 J

3
ODE PREDICTION & SIGNAL GENERATION

Running backward ODE to find corrected initial conditions...

NOW
T = 0
Asteroid detected at 76.3% threat level
Time to impact: 18 hours
←
Running ODE backward in time
Method: Lyapunov sensitivity analysis
Target: Conditions that lead to 20 km miss
-6MO
T - 6 months
Predicted safe asteroid position: [-2.3 km, +0.8 km, +1.1 km]
Required velocity correction: -0.8 cm/s (vertical)
ODE_PREDICT r_safe_trajectory, constraints="newtonian_mechanics + solar_gravity", target_outcome="20km_miss", timestep=backward, time_horizon=6_months → Correction vector: [-2.3 km, +0.8 km, +1.1 km, -0.008 m/s] → Natural mechanism: Comet close approach → Timing: T-6 months ± 2 weeks → Confidence: 94%
Signal Generation Energy Cost 0 J (Information only)

4
RETROCAUSAL SIGNAL TRANSMISSION (CTC)

Sending control signal backward through Closed Timelike Curve...

SIGNAL PARAMETERS:
Target: Asteroid orbital mechanics
Mechanism: Comet gravitational perturbation
Timing: Historical close approach (already recorded)
Effect: 2-3 km positional shift → 20 km miss at Earth
Confidence: 94%
CTC_SEND r_deflection_signal -> r_past_universe_state method: "gravitational_perturbation" source: "comet_encounter" correction: [-2.3 km, +0.8 km, +1.1 km] timing: T-6_months → Signal propagating backward through spacetime...

5
NOVIKOV SELF-CONSISTENCY VERIFICATION

Checking for temporal paradoxes and fixed-point solutions...

FIXED POINT
LOOP
✓
PARADOX
CYCLE
V(t+1)=1-V(t)
NOVIKOV_CHECK r_timeline, tolerance=0.01 Checking for paradoxes... ✓ Comet approach was historically recorded ✓ No "grandfather paradox" created ✓ Timeline forms self-consistent loop ✓ Signal arrival = signal history (no causality violation)

6
MULTIVERSE COLLAPSE TO SAFE OUTCOME

Collapsing superposition into single stable reality...

CCT_COLLAPSE r_multiverse, question_TSP="which_branch_avoids_impact", budget=r_available_energy Processing: Traversing Question Lattice... Branch W0: risk=0.15, entropy=0.19 ✓ Branch W1: risk=0.82, entropy=0.24 ✗ Branch W2: risk=0.80, entropy=0.23 ✗ Branch W3: risk=0.22, entropy=0.18 ✓ Branch W4: risk=0.18, entropy=0.17 ✓ Branch W5: risk=0.79, entropy=0.25 ✗ Branch W6: risk=0.20, entropy=0.19 ✓ Branch W7: risk=0.81, entropy=0.24 ✗ Selection criteria: entropy - (budget_factor × severity × 0.15) Optimal branch: W0 (lowest entropy after interference amplification)
Initializing CCT_DEFLECT protocol...