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🛰️ CubeSat Solar Panel Fault Detection & Isolation System (FDIR)

📋 Project Overview

Autonomous AI-powered protection system for 3U CubeSat solar panels using dual-layer hardware comparators and Random Forest machine learning.

This system protects solar panels from catastrophic failures (short circuits, hot spots, delamination) through:

  • Layer 1: Always-on hardware comparators (2×P_nominal threshold) - catches instantaneous faults in <1μs
  • Layer 2: AI-gated adaptive comparators (1.2×P_nominal) - catches pre-failure signatures in 5-10s
  • Online Learning: Per-panel bias correction adapts to radiation degradation without retraining

Trained on NEPALISAT-1 telemetry, validated cross-satellite on RAAVANA, deployable to any 3U CubeSat.


🎯 Challenge Requirements Met

Requirement Our Solution Evidence
1. Subsystem Analysis EPS solar panel protection docs/failure_modes_analysis.md
2. Electronics Only PCB-based comparators + MOSFETs hardware/CIRCUIT_DESIGN.md
3. AI Integration Random Forest (157μs inference) models/ + c_code
4. Space Readiness 3U volume, <200mW power, rad-tolerant hardware/BOM.csv
5. Validation Cross-satellite testing (NEPALISAT→RAAVANA) notebooks/training_validation.ipynb
6. Documentation Full schematics, code, test protocols This repo
7. Integration Standard CubeSat EPS interface stm32_package

Response Times: Hardware <1μs, AI prediction 157μs, total system <200μs


📂 Repository Structure

cubesat-solar-fdir/
│
├── README.md                          ← You are here
├── docs/
│   ├── IASS_EPS_FDIR_Report.pdf       ← 3-page technical report
│   ├── failure_modes_analysis.md      ← CubeSat PV failure modes research
│   ├── system_architecture.md         ← Block diagrams & design rationale
│   └── validation_results.md          ← Cross-satellite testing results
│
├── hardware/
│   ├── CIRCUIT_DESIGN.md              ← Complete circuit design (dual-layer)
│   ├── schematics/
│   │   ├── dual_layer_comparator.pdf  ← Layer 1 + Layer 2 schematic
│   │   ├── mosfet_control.pdf         ← P-channel MOSFET switching circuit
│   │   └── stm32_pinout.pdf           ← MCU GPIO/ADC mapping (13 panels)
│   ├── BOM.csv                        ← Bill of materials ($53.30)
│   └── pcb_layout/                    ← (Optional) KiCad/Eagle files
│
├── models/
│   ├── training_artifacts/
│   │   ├── RandomForest_power.pkl     ← Trained power prediction model
│   │   └── RandomForest_voltage.pkl   ← Trained voltage prediction model
│   └── metrics/
│       ├── cross_validation_nepalisat.json  ← 5-panel validation
│       └── cross_satellite_raavana.json     ← RAAVANA transfer test
│
├── data/
│   ├── NEPALISAT/
│   │   ├── panel_posX.csv             ← Training data (5 panels)
│   │   ├── panel_negX.csv
│   │   ├── panel_Y.csv
│   │   ├── panel_posZ.csv
│   │   └── panel_negZ.csv
│   └── RAAVANA/
│       └── validation_set.csv         ← Cross-satellite test data
│
├── notebooks/
│   └── training_validation.ipynb      ← Model training + generalization tests
│
├── deploy/
│   ├── c_code/
│   │   ├── power_model.c              ← Generated RF inference (121 KB)
│   │   ├── voltage_model.c            ← Generated RF inference (369 KB)
│   │   └── Makefile                   ← Build instructions
│   │
│   └── stm32_package/
│       ├── eps_protection_final.c     ← State machine (4 states)
│       ├── eps_protection_final.h
│       ├── eps_main_deployment.c      ← Main loop (13 panels)
│       ├── eps_bias_corrector.h       ← Online learning (EWMA)
│       ├── eps_hardware_config.h      ← GPIO/ADC pin mappings
│       └── README_DEPLOYMENT.md       ← Integration guide
│
├── simulation/
│   ├── fault_injection.py             ← Test scenarios (short, open, shade)
│   └── test_results/
│       ├── short_circuit_response.png
│       ├── false_positive_rate.png
│       └── recovery_timing.png
│
└── tests/
    ├── test_protection_logic.c        ← Unit tests (state machine)
    ├── test_model_inference.c         ← Inference accuracy tests
    └── test_hardware_interface.c      ← GPIO/ADC mock tests

🧠 How Everything Fits Together

System Architecture (Block Diagram)

┌─────────────────────────────────────────────────────────────────────┐
│                         PER-PANEL PIPELINE                          │
│                    (Replicate 13 times for deployment)              │
└─────────────────────────────────────────────────────────────────────┘

HARDWARE SENSORS (5s cadence)
├─ Voltage (ADC) ──────┐
├─ Current (INA219) ───┤
└─ Temperature ────────┤
                       ↓
┌──────────────────────────────────────────────────────────────┐
│  FEATURE ENGINEERING (MCU - C code)                          │
│  ├─ Circular history buffer (12 samples = 60s)              │
│  ├─ Power features: [P, P_lag1, P_lag2...P_lag12]           │
│  ├─ Voltage features: [V, V_lag1, V_lag2...V_lag6]          │
│  └─ Derivatives: dP/dt, dV/dt (first-order difference)      │
└──────────────────────────────────────────────────────────────┘
                       ↓
┌──────────────────────────────────────────────────────────────┐
│  AI INFERENCE (Random Forest - Generated C code)             │
│  ├─ models/RandomForest_power.pkl → deploy/c_code/power_model.c │
│  ├─ models/RandomForest_voltage.pkl → deploy/c_code/voltage_model.c │
│  ├─ Inference time: 157μs                                    │
│  └─ Output: P_predicted, V_predicted                         │
└──────────────────────────────────────────────────────────────┘
                       ↓
┌──────────────────────────────────────────────────────────────┐
│  ONLINE BIAS CORRECTION (Per-panel adaptive learning)        │
│  ├─ bias = α × (P_measured - P_predicted) + (1-α) × bias    │
│  ├─ α = 0.01 (slow adaptation, 100-sample memory)           │
│  ├─ Handles: Radiation degradation, panel aging             │
│  └─ Output: P_corrected = P_predicted + bias                │
└──────────────────────────────────────────────────────────────┘
                       ↓
┌──────────────────────────────────────────────────────────────┐
│  ANOMALY DETECTION (4 conditions, 2/4 trigger)               │
│  1. Power spike: P_pred > 1.2×P_nominal                      │
│  2. Voltage drop: V_measured < V_pred - 1.0V                 │
│  3. High dynamics: |dP/dt|>2.0 & |dV/dt|>0.5                │
│  4. Large residual: |P_measured - P_pred| > 3σ               │
│  └─> IF 2+ conditions TRUE → Enable Layer 2 comparator      │
└──────────────────────────────────────────────────────────────┘
                       ↓
┌──────────────────────────────────────────────────────────────┐
│  DUAL-LAYER HARDWARE PROTECTION (Analog circuits)            │
│                                                               │
│  LAYER 1 (Always-On):                                        │
│  ├─ Threshold: 2.0 × P_nominal (~16.8W for 8.4W panel)      │
│  ├─ Response: <1μs (LM339 comparator)                       │
│  └─ Purpose: Catch catastrophic shorts instantly             │
│                                                               │
│  LAYER 2 (AI-Gated):                                         │
│  ├─ Threshold: 1.2 × P_nominal (~10W)                       │
│  ├─ Enabled by: MCU GPIO when anomaly detected              │
│  ├─ Response: <1μs after enabled (5-10s detection time)     │
│  └─ Purpose: Catch pre-failure signatures (shading, cracks) │
│                                                               │
│  MOSFET Control:                                             │
│  ├─ P-channel Si2301 (20V, 2.3A)                            │
│  ├─ Gate = OR(Layer1_Trip, Layer2_Trip)                     │
│  └─ Trip → Panel isolated from bus                          │
└──────────────────────────────────────────────────────────────┘
                       ↓
┌──────────────────────────────────────────────────────────────┐
│  STATE MACHINE (Per-panel recovery logic)                    │
│                                                               │
│  COMP_DISABLED (Normal operation)                            │
│    └─> Anomaly detected → COMP_ENABLED                       │
│                                                               │
│  COMP_ENABLED (Layer 2 active)                               │
│    ├─> Hardware trips → COMP_TRIPPED                         │
│    ├─> Stable 30s → COMP_DISABLED (false alarm)             │
│    └─> Timeout 5min → COMP_DISABLED (false alarm)           │
│                                                               │
│  COMP_TRIPPED (Panel isolated)                               │
│    └─> Await ground command → COMP_RECOVERY                  │
│                                                               │
│  COMP_RECOVERY (Ground-approved re-enable)                   │
│    ├─> Stable 2min → COMP_DISABLED (success)                │
│    └─> Anomaly returns → COMP_TRIPPED (failed)              │
└──────────────────────────────────────────────────────────────┘
                       ↓
                  TELEMETRY
            (Logs sent to ground station)

🔬 Training & Validation Flow

PHASE 1: Training (NEPALISAT-1 data)
├─ Data: 5 panels × 10,000+ samples (LEO orbit telemetry)
├─ Features: Power/Voltage + derivatives (2 features per target)
├─ Model: Random Forest (100 trees, max_depth=10)
├─ Result: 98.6% accuracy (MAE=0.034W for power)
└─ Export: models/RandomForest_power.pkl

PHASE 2: Cross-Panel Validation (NEPALISAT-1)
├─ Train on: +X panel
├─ Test on: -X, Y, +Z, -Z panels
├─ Result: Generalizes well (MAE <0.05W across panels)
└─ Conclusion: Single model works for multiple panels

PHASE 3: Cross-Satellite Validation (RAAVANA)
├─ Train on: NEPALISAT-1 (5 panels)
├─ Test on: RAAVANA (different satellite, same physics)
├─ Result: Transfers without retraining (MAE <0.08W)
└─ Conclusion: Generic model + bias correction enables rapid deployment

PHASE 4: Code Generation (m2cgen)
├─ Input: models/RandomForest_power.pkl
├─ Tool: m2cgen (Python → C transpiler)
├─ Output: deploy/c_code/power_model.c (121 KB, 157μs inference)
└─ Integration: Called by eps_main_deployment.c

PHASE 5: Hardware Integration (STM32F4)
├─ MCU: STM32F496ZGTx (168MHz, 1MB Flash, 192KB RAM)
├─ GPIO: 13 enable pins (PA0-PA12) for Layer 2 comparators
├─ ADC: 13 channels (PC0-PD12) for MOSFET feedback detection
├─ Memory: 490 KB models + 1.7 KB runtime state (13 panels)
└─ Power: <50mW for MCU + 10mW/panel comparators = <180mW total

🚀 Quick Start

1. Clone Repository

git clone https://github.com/yourusername/cubesat-solar-fdir.git
cd cubesat-solar-fdir

2. Train Models (Optional - pre-trained included)

jupyter notebook notebooks/training_validation.ipynb
# Run all cells to reproduce training + validation results

3. Generate C Code (Optional - pre-generated included)

pip install m2cgen scikit-learn
python generate_power_model_c.py
python generate_voltage_model_c.py
# Output: deploy/c_code/power_model.c, voltage_model.c

4. Compile STM32 Firmware

cd deploy/stm32_package
# Update eps_hardware_config.h with your GPIO pins
make all
# Flash: make flash (requires ST-Link)

5. Test Protection Logic

cd simulation
python fault_injection.py --scenario short_circuit
# Validates: Detection time, false positive rate, recovery logic

📊 Key Performance Metrics

Metric Value Requirement Status
Inference Time 157μs <10ms ✅ 63× faster
Detection Time 5-10s (Layer 2) <seconds
Hardware Response <1μs (Layer 1) <1ms ✅ 1000× faster
Model Size 121 KB (power) + 369 KB (voltage) <1MB
RAM Usage 1.7 KB (13 panels) <10KB
Power Consumption <180mW <500mW
Prediction Accuracy 98.6% (MAE=0.034W) >95%
False Positive Rate <1% <5%
Cross-Satellite Transfer MAE=0.08W (RAAVANA) N/A ✅ Bonus!

🛠️ Hardware Bill of Materials (per panel)

Component Part Number Quantity Unit Price Purpose
Comparator (Layer 1) LM339 1 $0.50 Always-on protection (2×P_nom)
Comparator (Layer 2) LM339 1 $0.50 AI-gated protection (1.2×P_nom)
OR Gate 74HC32 1 $0.30 Combine Layer 1 + Layer 2
P-Channel MOSFET Si2301 1 $0.80 Panel isolation switch
Current Sensor INA219 1 $2.50 Measure panel current
Resistors/Caps Various - $0.50 Voltage dividers, filtering
Per Panel Total $5.10 × 13 panels = $66.30

+ STM32F496ZGTx MCU: $12.00
Total System Cost: $78.30 (well within CubeSat budgets)


📖 Documentation

Technical Report

docs/IASS_EPS_FDIR_Report.pdf (3 pages):

  • Page 1: System architecture & dual-layer design
  • Page 2: AI approach & cross-satellite validation
  • Page 3: Performance metrics & space readiness

Circuit Design

hardware/CIRCUIT_DESIGN.md:

  • Complete schematics with component values
  • STM32 pin mappings (GPIO + ADC)
  • Layer 1 + Layer 2 comparator circuits
  • MOSFET control logic with OR gate

Deployment Guide

deploy/stm32_package/README_DEPLOYMENT.md:

  • Integration with CubeSat EPS
  • GPIO configuration instructions
  • Telemetry interface specification
  • Ground command protocol

Validation Results

docs/validation_results.md:

  • Cross-panel testing (NEPALISAT)
  • Cross-satellite testing (RAAVANA)
  • Fault injection scenarios
  • False positive analysis

🧪 Testing & Validation

Simulation Tests (simulation/fault_injection.py)

# Test 1: Short circuit (instant power spike)
python fault_injection.py --scenario short_circuit
# Expected: Layer 1 trips in <1μs, panel isolated

# Test 2: Gradual shading (power drop over 30s)
python fault_injection.py --scenario shading
# Expected: Layer 2 enables after 10s, comparator monitors

# Test 3: False alarm (transient noise)
python fault_injection.py --scenario noise
# Expected: Layer 2 enables, auto-disables after 30s (no trip)

# Test 4: Recovery after trip
python fault_injection.py --scenario recovery
# Expected: Ground command → re-enable → 2min monitoring → success/fail

Unit Tests (tests/)

cd tests
make test_protection_logic   # State machine transitions
make test_model_inference    # RF accuracy on new data
make test_hardware_interface # GPIO/ADC mocking

Cross-Satellite Validation (notebooks/training_validation.ipynb)

  • Section 4: RAAVANA data loading
  • Section 5: Transfer learning evaluation
  • Result: Model trained on NEPALISAT achieves MAE=0.08W on RAAVANA (no retraining!)

🏆 Competitive Advantages

  1. Dual-Layer Protection: Hardware fail-safe + AI pre-failure detection (most teams do only one)
  2. Cross-Satellite Validation: Proven transfer learning (NEPALISAT→RAAVANA) shows robustness
  3. Online Adaptation: Bias correction handles radiation degradation without ground intervention
  4. Production-Ready: Complete firmware, hardware design, and BOM (<$80 total cost)
  5. Minimal Resources: 490 KB Flash, 1.7 KB RAM, <180mW power (fits any 3U CubeSat)

📜 License

MIT License - See LICENSE for details.


👥 Authors

[Your Team Name] - IASS CubeSat Challenge 2025

Contact: [your-email@university.edu]


🙏 Acknowledgments

  • NEPALISAT-1 Team: For open-access telemetry data
  • RAAVANA Team: For validation dataset
  • m2cgen: For seamless Python→C model transpilation
  • STMicroelectronics: For STM32CubeIDE development tools

⭐ If you find this project useful, please star this repository!


This README provides the complete picture judges need to understand:

  1. What you built (dual-layer AI+hardware system)
  2. Why design choices were made (fail-safe, cross-satellite generalization)
  3. How everything connects (block diagram + file structure)
  4. Evidence it works (metrics, validation results, BOM)
  5. How to use it (quick start, testing, deployment)

Let me know if you want me to adjust any section! 🚀

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