Diagnosis and Fault-Tolerant Control of Nonlinear Systems
Date
2026-06-18
Authors
Journal Title
Journal ISSN
Volume Title
Publisher
Echahid Cheikh Larbi Tebessi University- Tebessa
Abstract
The demand for reliable, autonomous operation in complex, safety-critical non-
linear systems such as Unmanned Aerial Vehicles (UAVs) necessitates advanced
Fault-Tolerant Control (FTC) capabilities. Conventional FTC methods struggle
with system non-linearity and lack the adaptive performance required for robust
operation. Conversely, purely AI-based approaches, while highly adaptive, suffer
from a lack of formal safety guarantees and increased computational complexity.
This dissertation bridges this critical gap by proposing and validating a novel
Hybrid Fault-Tolerant Control (HFTC) strategy that strategically integrates the
verifiable rigor of conventional control with the optimizing power of metaheuristic
techniques. The core of this framework is a robust Sliding Mode Control (SMC)
architecture enhanced by a proposed Enhanced Triple Power Reaching Law (ET-
PRL), which provides superior chattering attenuation and accelerated finite-time
convergence. The HFTC architecture employs a unique hybrid compensation strat-
egy that includes an Online Diagnosis component, where a conventional extended
kalman filter (EKF-based) fault detection and identification (FDI) unit provides
real-time fault estimates, and an Offline Optimization component, where the par-
ticle swarm optimization (PSO) algorithm is utilized to pre-compute and store a
"Bank of Parameters" for numerous actuator fault scenarios. The efficacy of this
framework is rigorously validated through a comprehensive case study on a UAV
quadrotor subjected to severe Loss of Effectiveness (LOE) actuator faults. MAT-
LAB/Simulink simulations, including challenging helical and square trajectory
maneuvers, quantitatively demonstrate the superior performance of the HFTC-
ETPRL system, confirming its ability to maintain stability and achieve minimal
tracking error (e.g., up to a 50% reduction in Peak Deviation compared to bench-
mark controllers), underscoring the benefits of non-iterative, pre-optimized recon-
figuration. In synthesis, this research advances the state-of-the-art by validating
an efficient and high-performance hybrid solution that addresses the fundamental
trade-off between robustness and adaptability.
Description
Keywords
Fault-Tolerant Control (FTC), Sliding Mode Control (SMC), En- hanced Triple Power Reaching Law (ETPRL), Particle Swarm Optimization (PSO), Extended Kalman Filter (EKF), Unmanned Aerial Vehicle (UAV), Loss of Effectiveness (LOE)