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π Artemis II Human-in-the-Loop Crew Performance Simulator
Forward-looking synthetic modeling of crew physiology and cognitive reliability for NASAβs planned Artemis II lunar flyby mission.
π§ Overview
This project simulates human cognitive performance across the full Artemis II mission timeline.
Unlike traditional aerospace simulations that focus on hardware systems, this framework models the human system:
- Sleep pressure & circadian rhythm
- Cognitive performance
- Error probability (CREAM)
- COβ cognitive effects
- Radiation exposure
- Countermeasures (caffeine, naps, light therapy)
- Team workload fairness
- Mission-phase stress
All outputs are fully synthetic and generated via Monte Carlo simulation.
π° Figure 1 β Artemis II Mission Trajectory with Crew Performance Overlay
What this shows
Top panel:
- Distance from Earth across the 15-step Artemis II sequence
- Outbound transit
- Lunar flyby (6,513 km)
- Trans-Earth return
- Magnetosphere boundary
Bottom panel:
- Cognitive performance of each crew member
- Concern threshold (70%)
- Critical threshold (65%)
- Mission phase shading
Why it matters
This figure demonstrates that:
- Performance dips align with circadian troughs
- High-workload phases amplify fatigue
- Lunar flyby timing interacts with biological rhythms
- Deep-space segments show stable but cyclic cognitive oscillations
This is a direct example of orbital context interacting with human reliability.
π§ Figure 2 β Peak Performance Windows (Top 20)
What this shows
- Top 20 predicted high-performance windows
- Role-differentiated optimal task intervals
- Ranked across mission time
Why it matters
This enables:
- Scheduling cognitively demanding tasks
- Aligning procedures with peak biological readiness
- Pre-mission task optimization
It transforms physiology into operational decision-support.
β Figure 3 β Workload Distribution Fairness (Gini Coefficient)
What this shows
- Gini coefficient across mission time
- 0 = equal workload distribution
- 1 = highly unequal workload
- Concern threshold at 0.30
Why it matters
Unequal workload distribution:
- Increases cognitive stress on specific crew members
- Amplifies fatigue accumulation
- Raises downstream error probability
This introduces team-level reliability modeling, not just individual modeling.
π Figure 4 β Sensitivity Analysis (Countermeasures & Environment)
Scenarios tested:
- Baseline
- High COβ
- No caffeine
- No countermeasures
- Sleep shift Β±2 hours
Outputs shown:
- Mean cognitive performance
- % time below critical threshold
- Mean error probability
Why it matters
This shows:
- Removing countermeasures significantly increases risk
- High COβ environments measurably degrade reliability
- Sleep phase misalignment increases error exposure
This supports countermeasure evaluation before flight.
π₯ Figure 5 β Mission Risk Heatmap (CREAM Error Probability)
What this shows
- Hour-of-day vs mission-day error probability
- Higher intensity = higher predicted error risk
Why it matters
This reveals:
- Circadian-linked reliability bands
- Early-mission vulnerability
- Risk clustering during workload spikes
It provides a temporal reliability fingerprint of the mission.
π¨βπ Figure 6 β Role-Differentiated Workload & Performance
What this shows
For each role (CDR, PLT, MS1, MS2):
- Workload curve
- Cognitive performance
- Nap interventions
- Threshold overlays
Why it matters
This demonstrates:
- Different roles accumulate fatigue differently
- Workload asymmetry affects performance
- Countermeasure timing changes recovery curves
This supports role-aware mission planning.
π Figure 7 β Mission Timeline Physiological Overview
Includes:
A. Mean performance + 90% CI
B. Homeostatic sleep drive
C. Allostatic load
D. Caffeine pharmacokinetics
E. Cabin COβ levels
F. CREAM control mode by mission phase
Why it matters
This integrates:
- Biological rhythms
- Environmental stressors
- Countermeasures
- Reliability modes
into a single systems-level view of the mission.
π§ What Makes This Structurally Unique
This simulator integrates:
- Sleep science
- Human reliability analysis (CREAM)
- Environmental modeling
- Team fairness metrics
- Monte Carlo uncertainty
- Mission-phase annotation
There is no known open-source framework that combines:
Human physiology + reliability modeling + orbital context + countermeasure sensitivity + team fairness
for Artemis-class missions.
π― Intended Users
π Students
Human factors, aerospace systems, Monte Carlo modeling.
π§ Human Factors Engineers
Fatigue-aware task scheduling, countermeasure evaluation.
π Data Scientists
Synthetic multi-agent time-series dataset.
π° Space Systems Engineers
Human-in-the-loop risk modeling.
β Disclaimer
This is a research-grade simulation framework.
It is not:
- A NASA operational tool
- A medical diagnostic system
- A flight safety authority
All data is synthetic.
π€ Author
DBbun LLC
2026
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