Adaptive Nonlinear Gain Approximation of a Robust Nonlinear Controller to Handle Uncertain Disturbances for UAV Systems Using Neural Networks
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Date
2025
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Library Information Services, COMSATS University Islamabad, Lahore Campus
Abstract
The quadrotor unmanned aerial vehicle (UAV) has been a part of scientific studies
owing to its applications in military, agriculture, infrastructure and construction, and
environmental monitoring and conservation. However, its control design is challenging
due to its nonlinear underactuated dynamics, external disturbances, parametric
uncertainties, and the aerodynamic variations encountered during flight operations.
Sliding mode control (SMC) is the most widely used control technique for handling
nonlinear dynamics in the presence of external disturbances and modeling uncertainties.
However, conventional SMC requires a priori knowledge of the upper bound on the
overall disturbance at all times. Usually, these upper bounds on disturbances are
derived from past data, environmental conditions, and empirical modeling; therefore, a
conservative bound is used in SMC design, leading to high control effort and draining
more energy from the system. To address this issue, adaptive sliding mode control
(ASMC) strategies based on a neural network (NN) are presented in this dissertation.
Neural networks are recognized as the leading approach to intelligent computation
and are highly effective in handling nonlinearity, fault tolerance, adaptation, and
continuous online learning. In this research, NN-based ASMC strategies are presented
for a quadrotor UAV to improve flight performance by online estimation of adaptive
modulation gain in response to variations in disturbance magnitude. Different neural
network schemes are employed, including feed-forward neural networks (FNNs) using
backpropagation (BP) and Levenberg-Marquardt (LM) algorithms for optimization,
and a radial basis function neural network (RBFNN) with a Gaussian activation
function, to adaptively estimate the modulation gains. Furthermore, the stability
analysis of the proposed controllers is proven using Lyapunov theory.
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Keywords
Department of Electrical Engineering, FA23, Electrical Engineering, UAV systems, Robust nonlinear control, Neural networks, Adaptive control, Disturbance rejection, Dr. Mirza Tariq Hamayun