Trajectory Tracking Control for Quadrotor Formation Subject to Environmental and Model Uncertainties
This paper proposes a robust adaptive global control approach for quadrotor aircraft formation system based on RBF neural network against parametric uncertainties and bounded external disturbances for the quadrotor aircraft sys-tem. The actual controller consists of neural network controller in the...
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Published in | Proceedings of ... IEEE International Conference on Unmanned Systems (Online) pp. 829 - 834 |
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Main Authors | , , , |
Format | Conference Proceeding |
Language | English |
Published |
IEEE
28.10.2022
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Subjects | |
Online Access | Get full text |
ISSN | 2771-7372 |
DOI | 10.1109/ICUS55513.2022.9987194 |
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Abstract | This paper proposes a robust adaptive global control approach for quadrotor aircraft formation system based on RBF neural network against parametric uncertainties and bounded external disturbances for the quadrotor aircraft sys-tem. The actual controller consists of neural network controller in the approximate domain and robust controller outside the approximate domain. In order to ensure that all the signals of the closed-loop system are globally consistent and ultimately bounded, a smooth switching function is introduced to realize the smooth switching among controllers. What is more, Lyapunov function and Barbalat lemma are used to prove the stability of the nonlinear quadrotor aircraft formation system, and analyze the system stability strictly. Finally, we apply the proposed controller in MATLAB and Simulink software platforms, and analyze the numerical results. |
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AbstractList | This paper proposes a robust adaptive global control approach for quadrotor aircraft formation system based on RBF neural network against parametric uncertainties and bounded external disturbances for the quadrotor aircraft sys-tem. The actual controller consists of neural network controller in the approximate domain and robust controller outside the approximate domain. In order to ensure that all the signals of the closed-loop system are globally consistent and ultimately bounded, a smooth switching function is introduced to realize the smooth switching among controllers. What is more, Lyapunov function and Barbalat lemma are used to prove the stability of the nonlinear quadrotor aircraft formation system, and analyze the system stability strictly. Finally, we apply the proposed controller in MATLAB and Simulink software platforms, and analyze the numerical results. |
Author | Wang, Jinbo Chen, Lin Ma, Zhenwei Chen, Hongbo |
Author_xml | – sequence: 1 givenname: Zhenwei surname: Ma fullname: Ma, Zhenwei email: mazhw6@mail2.sysu.edu.cn organization: School of Systems Science and Engineering, Sun Yat-Sen University,Guangzhou,China – sequence: 2 givenname: Lin surname: Chen fullname: Chen, Lin email: chenlin87@mail2.sysu.edu.cn organization: School of Systems Science and Engineering, Sun Yat-Sen University,Guangzhou,China – sequence: 3 givenname: Jinbo surname: Wang fullname: Wang, Jinbo email: wangjinbo@mail.sysu.edu.cn organization: School of Systems Science and Engineering, Sun Yat-Sen University,Guangzhou,China – sequence: 4 givenname: Hongbo surname: Chen fullname: Chen, Hongbo email: chenhongbo@mail.sysu.edu.cn organization: School of Systems Science and Engineering, Sun Yat-Sen University,Guangzhou,China |
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Snippet | This paper proposes a robust adaptive global control approach for quadrotor aircraft formation system based on RBF neural network against parametric... |
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SubjectTerms | Adaptive robust control Aircraft Closed loop systems Global controller Military aircraft Neural networks Quadrotor formation RBF neural network Stability analysis Switches Uncertainty |
Title | Trajectory Tracking Control for Quadrotor Formation Subject to Environmental and Model Uncertainties |
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