The attitude control of UAV in carrier landing based on ADRC

In this paper, the problem of unmanned aerial vehicle(UAV) pitch angle control is considered. We employ a method of active disturbance rejection control(ADRC) to solve the problem. Firstly, UAV model including windy and windless condition and disturbance model are introduced. Next, ADRC-based contro...

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Published in2016 IEEE Chinese Guidance, Navigation and Control Conference (CGNCC) pp. 832 - 837
Main Authors Yu, Yue, Wang, Honglun, Shao, Xingling, Huang, Yu
Format Conference Proceeding
LanguageEnglish
Published IEEE 01.08.2016
Subjects
Atmospheric modeling
Bandwidth
Benchmark testing
Mathematical model
Observers
Wind
Online AccessGet full text
DOI10.1109/CGNCC.2016.7828893

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Abstract In this paper, the problem of unmanned aerial vehicle(UAV) pitch angle control is considered. We employ a method of active disturbance rejection control(ADRC) to solve the problem. Firstly, UAV model including windy and windless condition and disturbance model are introduced. Next, ADRC-based controller is designed for UAV model. Finally, a series of numerical simulations are presented. The simulation results demonstrate that ADRC has an excellent performance in terms of estimation of states and internal and external disturbance, attitude tracking, disturbance rejection and robustness to model uncertainties.
AbstractList In this paper, the problem of unmanned aerial vehicle(UAV) pitch angle control is considered. We employ a method of active disturbance rejection control(ADRC) to solve the problem. Firstly, UAV model including windy and windless condition and disturbance model are introduced. Next, ADRC-based controller is designed for UAV model. Finally, a series of numerical simulations are presented. The simulation results demonstrate that ADRC has an excellent performance in terms of estimation of states and internal and external disturbance, attitude tracking, disturbance rejection and robustness to model uncertainties.
Author Yu, Yue
Wang, Honglun
Shao, Xingling
Huang, Yu
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  givenname: Yu
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  fullname: Huang, Yu
  email: hy5154@163.com
  organization: School of Automation Science and Electrical Engineering, Beihang University, Beijing, 100191 China
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Snippet In this paper, the problem of unmanned aerial vehicle(UAV) pitch angle control is considered. We employ a method of active disturbance rejection control(ADRC)...
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SubjectTerms Atmospheric modeling
Bandwidth
Benchmark testing
Mathematical model
Observers
Wind
Title The attitude control of UAV in carrier landing based on ADRC
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