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article · IEEE Access

Robust Tracking Control for Quadrotor UAV With External Disturbances and Uncertainties Using Neural Network Based MRAC

202496 citationsOpen accessAddis Ababa University

In plain language

Quadrotor unmanned aerial vehicles often face operational challenges from wind, external disturbances, and internal parameter changes. To improve flight stability, an intelligent control framework combines Model Reference Adaptive Control with artificial neural networks. The system relies on a singularity-free dynamic model formulated through Newton-Quaternion mathematics. Training data generated from conventional adaptive control is used to train a feed-forward neural network for position estimation and a recurrent neural network for attitude control. An online learning algorithm continuously updates these network parameters during flight. Numerical simulations testing nominal conditions, matched and unmatched disturbances, and parametric shifts demonstrated superior trajectory tracking and disturbance rejection compared to standard linear quadratic regulators and conventional adaptive systems. The control signals remained smooth and minimal, suggesting strong potential for practical, real-time quadrotor operations.

Key takeaways

  • A neural network-based Model Reference Adaptive Control framework was designed to improve quadrotor trajectory tracking under disturbances and parameter shifts.
  • Feed-forward and recurrent neural networks manage position controller parameter estimation and attitude control, updated via real-time online learning.
  • Simulation tests showed better tracking performance and disturbance rejection compared with Linear Quadratic Regulator and conventional adaptive controllers.
  • The controller generated smooth and minimal control signals, supporting functional safety and efficient operation.

Why it matters

Unmanned aerial vehicles must navigate unpredictable environments such as gusty winds without losing stability or consuming excessive power. By combining neural networks with adaptive flight control, quadrotors can self-adjust to sudden physical disturbances and internal variations. This delivers more dependable, efficient autonomous flight, which is essential for safely operating drones across complex operational conditions.

Commercialisation angle

This controller could benefit commercial drone manufacturers, flight software developers, and autonomous inspection operators seeking robust autonomous flight in unstable weather. Because the findings are currently demonstrated solely through numerical simulations rather than hardware flight tests, the technology remains at an early, applied simulation stage. Further real-world validation on physical quadrotor platforms is necessary before integration into commercial flight management systems.

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Abstract

In this paper, an intelligent Model Reference Adaptive Control (MRAC) based on a neural network is proposed for robust tracking control of quadrotor UAV under external disturbances and parameter variations. First, the singularity-free dynamic model of the quadrotor is developed using Newton-Quaternion formalism. Then, conventional MRAC is designed to generate training data. With the generated data, the Feed Forward Neural Network (FFNN) and Recurrent Neural Network (RNN) are trained offline to get an initial set of network parameters for position controller parameters estimation and attitude control of the quadrotor, respectively, and an online learning algorithm is developed to update those network parameters in real-time. Finally, the performance of the designed Neural network-based MRAC has been evaluated using a numerical simulation in a nominal scenario and by introducing parametric variation and external disturbances as matched and unmatched uncertainties into the system. The simulation results show that the proposed controller has a better tracking performance and disturbance rejection capability compared with the Linear Quadratic Regulator (LQR) and conventional MRAC. Furthermore, the utilized control efforts are minimal and smooth proving functional safety and economical use of the controller. Therefore, the suggested controller is feasible for real-time implementation of the quadrotor UAV.

Research topics

  • Adaptive Control of Nonlinear Systems
  • Aerospace Engineering and Control Systems
  • Advanced Control Systems Design

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DOI: 10.1109/access.2024.3374894

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