4.5 Article

Path-Following Control of Small Fixed-Wing UAVs under Wind Disturbance

期刊

DRONES
卷 7, 期 4, 页码 -

出版社

MDPI
DOI: 10.3390/drones7040253

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fixed-wing UAV; path following; GSISM plus RBF S-Plane controller; wind disturbances

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To address the issues of low following accuracy and weak anti-disturbance ability in 3D path-following control for small fixed-wing UAVs, a Globally Stable Integral Sliding Mode Radial Basis Function S-Plane (GSISM+RBF S-Plane) controller is designed. The controller adopts an inner and outer loop mode, with the outer loop using Globally Stable Integral Sliding Mode (GSISM) control and the inner loop using S-Plane control. An RBF neural network is used to estimate unknown disturbances in the model. Through simulation and comparative experiments, it is demonstrated that the GSISM+RBF S-Plane controller achieves accurate path tracking and exhibits good control and anti-disturbance performance compared to other controllers.
Aiming at the problems of low following accuracy and weak anti-disturbance ability in the three-dimensional path-following control of small fixed-wing Unmanned Aerial Vehicles (UAV), a Globally Stable Integral Sliding Mode Radial Basis Function S-Plane (GSISM+RBF S-Plane) controller is designed. The controller adopts the inner and outer loop mode, the outer loop adopts the Globally Stable Integral Sliding Mode (GSISM) control, and the inner loop adopts the S-Plane control. At the same time, the unknown disturbance in the model is estimated via an RBF neural network. Firstly, the outer loop controller is designed based on the GSISM, and its stability is proved using the Lyapunov theory. Then, the S-Plane controller is designed for the instruction signal of the inner loop. Considering the complexity of the derivation in the S-Plane controller, a second-order differentiator is introduced. Finally, considering the problem of external wind disturbance, the controller is modeled, studied, and processed in order to better reflect the impact of real external wind on UAV path following. Finally, the Globally Stable Sliding Mode (GSSM) control and Globally Stable Integral Sliding Mode S-Plane (GSISM S-Plane) control are used for a comparative experiment. The simulation results show that the designed GSISM+RBF S-Plane controller can accurately track the ideal path compared with the GSSM and GSISM S-Plane controller, and it has good control performance and anti-disturbance performance.

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