A physics-guided NARX-inspired network for accurate roll and pitch prediction of quadrotor UAVs

Purpose To develop a lightweight and physically interpretable approach for accurate one-step quadrotor attitude prediction. The study aims to reduce the learning burden of purely data-driven models by incorporating first-order rotational kinematics into a NARX-inspired neural architecture while retaining the ability to learn nonlinear dynamics and modeling errors. Design/methodology/approach A Physics-Guided NARX-inspired (PG-NARX) architecture is proposed, combining learnable autoregressive state propagation, a trainable physics-guided kinematic branch initialized using first-order rotational kinematics, and a neural residual branch. The approach is evaluated using flight-wise partitioned PX4-Gazebo Software-in-the-Loop data. PG-NARX is compared with MLP, NARX-inspired, Persistence, and Kinematic baselines using an unseen test trajectory, computational measurements, and angular-velocity noise experiments. Findings PG-NARX achieves roll and pitch RMSE values of 0.0206 rad and 0.0098 rad, with corresponding R2 values of 0.9558 and 0.9880. Compared with the Kinematic baseline, it reduces clean-test roll and pitch RMSE by approximately 10.8% and 17.6%, respectively. The model contains 18,602 trainable parameters and achieves a measured inference latency of 0.2667 ms. Additional experiments indicate relatively consistent performance under zero-mean Gaussian angular-velocity noise. Research limitations/implications The evaluation is limited to simulated PX4-Gazebo Software-in-the-Loop flight data and one-step attitude prediction, with roll and pitch as the primary targets. The results therefore do not establish performance under real-flight conditions, longer-horizon prediction, or more complex aerodynamic effects. Future research should validate the approach on real UAV hardware, investigate multi-step prediction and additional attitude states, and evaluate robustness across different flight conditions, disturbances, and sensor characteristics. Originality/value The study introduces a lightweight PG-NARX architecture that explicitly integrates first-order rotational kinematics into a NARX-inspired predictor through a trainable physics-guided branch and neural residual learning. Unlike purely data-driven NARX approaches, the proposed formulation assigns predictable short-term rotational behavior to a physics-guided component while allowing the neural network to learn remaining discrepancies. The resulting architecture provides a practical balance among prediction accuracy, computational efficiency, and physical interpretability for one-step quadrotor attitude prediction.

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Publication Details

Journal
International Journal of Intelligent Unmanned Systems
Published
2026-10-28
DOI
https://doi.org/10.1108/ijius-07-2026-0369
Primary Topic
Aerospace and Aviation Technology
Type
article
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article

A physics-guided NARX-inspired network for accurate roll and pitch prediction of quadrotor UAVs

Thịnh Minh Nguyễn, Khoa Dang Nguyen, Thang Van Nguyen, Van Thi Tran et al.
4 links
International Journal of Intelligent Unmanned Systems
Aerospace and Aviation Technology
article

A physics-guided NARX-inspired network for accurate roll and pitch prediction of quadrotor UAVs

Thịnh Minh Nguyễn, Khoa Dang Nguyen, Thang Van Nguyen, Van Thi Tran, Tung Thanh Bui
article en

Abstract

Purpose To develop a lightweight and physically interpretable approach for accurate one-step quadrotor attitude prediction. The study aims to reduce the learning burden of purely data-driven models by incorporating first-order rotational kinematics into a NARX-inspired neural architecture while retaining the ability to learn nonlinear dynamics and modeling errors. Design/methodology/approach A Physics-Guided NARX-inspired (PG-NARX) architecture is proposed, combining learnable autoregressive state propagation, a trainable physics-guided kinematic branch initialized using first-order rotational kinematics, and a neural residual branch. The approach is evaluated using flight-wise partitioned PX4-Gazebo Software-in-the-Loop data. PG-NARX is compared with MLP, NARX-inspired, Persistence, and Kinematic baselines using an unseen test trajectory, computational measurements, and angular-velocity noise experiments. Findings PG-NARX achieves roll and pitch RMSE values of 0.0206 rad and 0.0098 rad, with corresponding R2 values of 0.9558 and 0.9880. Compared with the Kinematic baseline, it reduces clean-test roll and pitch RMSE by approximately 10.8% and 17.6%, respectively. The model contains 18,602 trainable parameters and achieves a measured inference latency of 0.2667 ms. Additional experiments indicate relatively consistent performance under zero-mean Gaussian angular-velocity noise. Research limitations/implications The evaluation is limited to simulated PX4-Gazebo Software-in-the-Loop flight data and one-step attitude prediction, with roll and pitch as the primary targets. The results therefore do not establish performance under real-flight conditions, longer-horizon prediction, or more complex aerodynamic effects. Future research should validate the approach on real UAV hardware, investigate multi-step prediction and additional attitude states, and evaluate robustness across different flight conditions, disturbances, and sensor characteristics. Originality/value The study introduces a lightweight PG-NARX architecture that explicitly integrates first-order rotational kinematics into a NARX-inspired predictor through a trainable physics-guided branch and neural residual learning. Unlike purely data-driven NARX approaches, the proposed formulation assigns predictable short-term rotational behavior to a physics-guided component while allowing the neural network to learn remaining discrepancies. The resulting architecture provides a practical balance among prediction accuracy, computational efficiency, and physical interpretability for one-step quadrotor attitude prediction.

International Journal of Intelligent Unmanned Systems
Vietnam National University Ho Chi Minh City (VN), Vietnam National University, Hanoi (VN), Hanoi University of Civil Engineering (VN), Federal Ministry of Labour and Social Affairs (DE), Research Institute for Labour and Social Affairs (CZ), University of Labor and Social Affairs (VN)
Openalex Percentile: Top 19%
Aerospace and Aviation Technology
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