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To address the challenges posed by flight envelope limitation, external disturbances, model uncertainties and actuator failures in quadrotor unmanned aerial vehicles (UAVs), we propose an adaptive neural attitude control method that incorporates a Nussbaum function and nonlinear disturbance observer (NDO). By designing the Nussbaum function, we effectively address potential actuator failures while leveraging the NDO enables us to employ feedforward compensation strategy to mitigate perturbation effects. To handle the flight envelope limitation and model uncertainties, we introduce a nonlinear state-dependent function (NSDF) and neural networks (NNs), respectively. The NSDF is utilized to directly constrain the attitude, while the NNs are constructed to estimate the unknown components. Simulation results demonstrate that this approach successfully addresses the flight envelope limitation and maintains robust tracking performance even in the presence of external disturbances, model uncertainties and actuator failures in the controlled system.
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Yan‐Jun Liu
Liaoning University of Technology
Benke Gao
Liaoning University of Technology
Dengxiu Yu
Ministry of Public Security of the People's Republic of China
IEEE Transactions on Systems Man and Cybernetics Systems
Northwestern Polytechnical University
Liaoning University of Technology
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Liu et al. (Wed,) studied this question.
synapsesocial.com/papers/6a153e40d64fa333899f6a99 — DOI: https://doi.org/10.1109/tsmc.2025.3534986