z-logo
open-access-imgOpen Access
Stall Prediction in Quadcopters with SHAP-Based Explainability and a Novel Flight Dynamics Dataset
Author(s) -
Vatsal Siotia,
Ruppikha Sree Shankar,
Vishnu G Nair
Publication year - 2025
Publication title -
ieee access
Language(s) - English
Resource type - Magazines
SCImago Journal Rank - 0.587
H-Index - 127
eISSN - 2169-3536
DOI - 10.1109/access.2025.3611165
Subject(s) - aerospace , bioengineering , communication, networking and broadcast technologies , components, circuits, devices and systems , computing and processing , engineered materials, dielectrics and plasmas , engineering profession , fields, waves and electromagnetics , general topics for engineers , geoscience , nuclear engineering , photonics and electrooptics , power, energy and industry applications , robotics and control systems , signal processing and analysis , transportation
Unmanned Aerial Vehicles (UAVs), particularly quadcopters, are increasingly deployed in high-stakes operations including defense, tactical surveillance, disaster response, and GPS-denied missions. However, aerodynamic stall—caused by conditions like vortex ring state or rotor stall—remains a critical failure mode that can lead to sudden lift loss and catastrophic crashes. This study presents a hybrid stall prediction framework that unifies physics-informed synthetic data generation, interpretable machine learning, and embedded rule-based logic for real-time, onboard risk assessment. A custom simulator was developed to generate 25,921 stall-prone flight states by modeling key parameters such as throttle, vertical speed, blade angle of attack (AoA), airspeed, disc loading, and thrust-to-weight ratio. Using this dataset, an XGBoost classifier was trained for binary classification with two output classes: stall and non-stall, and optimized via threshold tuning and SMOTE-based class balancing. Using this dataset, an XGBoost classifier achieved 0.97 precision, 0.98 recall, 0.98 F1-score, and 0.96 accuracy for stall prediction after integration with domain-specific rules. SHapley Additive exPlanations (SHAP) values were applied to provide transparent, instance-level justifications, revealing that throttle, VRS, and disc loading were consistently the top contributors to stall predictions. In parallel, domain-specific aerodynamic rules—such as critical AoA and high disc loading thresholds—were deployed to catch edge cases such as near-threshold predictions, ambiguous vortex ring state regions, or unseen aerodynamic configurations. This modular system is designed for compatibility with onboard processors like Raspberry Pi, enabling real-time deployment even in resource-constrained environments. It supports frugal innovation without compromising safety, making it suitable for stealth drones, ISR swarms, payload-carrying UAVs, and companion-computer-based quadcopters. By combining data-driven predictions with physics-aware rule triggers, the system reduces false negatives and false positives, improving reliability in mission-critical conditions. Ultimately, this work pushes drone autonomy toward proactive, explainable, and hardware-efficient safety mechanisms—where UAVs not only predict aerodynamic stall but also justify it in real time.

The content you want is available to Zendy users.

Already have an account? Click here to sign in.
Having issues? You can contact us here
Accelerating Research

Address

John Eccles House
Robert Robinson Avenue,
Oxford Science Park, Oxford
OX4 4GP, United Kingdom