Date of Award
5-2026
Document Type
Thesis
Degree Name
Master of Science (MS)
Department
Aerospace, Physics, and Space Sciences
First Advisor
Camilo A. Riano-Rios
Second Advisor
Madhur Tiwari
Third Advisor
Ryan T. White
Fourth Advisor
Donald Platt
Abstract
Fault detection in aircraft is traditionally handled through redundant hardware and comparison algorithms to detect failures. Alternatives like model-based residual generation and data-driven approaches such as supervised fault classification and unsupervised anomaly detection have been explored, but they suffer from practical limitations; model-based methods require accurate system models, and data-driven methods have large constraints on the data limiting scalability and adaptability. This work presents a purely data-driven neural network architecture featuring a custom first layer designed for real-time fault detection where the weights and biases of this layer are used to detect faults. The network requires zero supervision and complements existing redundant-sensor systems by extracting fault-relevant features directly from sensor data. Statistical analysis shows a strong correlation between network weight changes and failure severity, supporting its effectiveness. A demonstration flight case study further validates the system’s real-time applicability. This work offers a scalable, low-overhead solution that bridges critical gaps in current aircraft fault detection strategies, enhancing reliability and operational safety.
Recommended Citation
Chen, George Harrison, "Aircraft Fault Detection via Weight and Bias Analysis of a Custom First Neural Network Layer" (2026). Theses and Dissertations. 1616.
https://repository.fit.edu/etd/1616
Included in
Artificial Intelligence and Robotics Commons, Navigation, Guidance, Control and Dynamics Commons