Attitude tracking control for quadrotor UAVs based on extremum seeking

A robust control method based on extremum seeking is proposed for the attitude tracking problem of quadrotor UAV with uncertainty. Firstly, a nonlinear attitude model of a four rotor UAV was established, and considering the uncertainty of model parameters, a robust controller was designed to ensure...

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Main Authors: GUO Dali, ZHAO Zhongyuan, LUO Zijuan
Format: Article
Language:zho
Published: POSTS&TELECOM PRESS Co., LTD 2023-12-01
Series:智能科学与技术学报
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Online Access:http://www.cjist.com.cn/thesisDetails#10.11959/j.issn.2096-6652.202337
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author GUO Dali
ZHAO Zhongyuan
LUO Zijuan
author_facet GUO Dali
ZHAO Zhongyuan
LUO Zijuan
author_sort GUO Dali
collection DOAJ
description A robust control method based on extremum seeking is proposed for the attitude tracking problem of quadrotor UAV with uncertainty. Firstly, a nonlinear attitude model of a four rotor UAV was established, and considering the uncertainty of model parameters, a robust controller was designed to ensure the dynamic boundedness of tracking errors. Secondly, a learning-based controller was designed by combining a robust controller with a model-free learning algorithm, which automatically and iteratively adjusted the feedback gain of the robust controller and optimized the expected performance cost function online. Finally, numerical simulations were performed using MATLAB, which demonstrated a reduction of 0.246 in the steady-state tracking error of the proposed control method compared to the classical robust control method. This result confirms the robustness and superiority of the proposed method.
format Article
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issn 2096-6652
language zho
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publisher POSTS&TELECOM PRESS Co., LTD
record_format Article
series 智能科学与技术学报
spelling doaj-art-796800a0cc03440095ff550b3d836bcb2025-08-20T02:13:41ZzhoPOSTS&TELECOM PRESS Co., LTD智能科学与技术学报2096-66522023-12-01548649348702375Attitude tracking control for quadrotor UAVs based on extremum seekingGUO DaliZHAO ZhongyuanLUO ZijuanA robust control method based on extremum seeking is proposed for the attitude tracking problem of quadrotor UAV with uncertainty. Firstly, a nonlinear attitude model of a four rotor UAV was established, and considering the uncertainty of model parameters, a robust controller was designed to ensure the dynamic boundedness of tracking errors. Secondly, a learning-based controller was designed by combining a robust controller with a model-free learning algorithm, which automatically and iteratively adjusted the feedback gain of the robust controller and optimized the expected performance cost function online. Finally, numerical simulations were performed using MATLAB, which demonstrated a reduction of 0.246 in the steady-state tracking error of the proposed control method compared to the classical robust control method. This result confirms the robustness and superiority of the proposed method.http://www.cjist.com.cn/thesisDetails#10.11959/j.issn.2096-6652.202337quadrotor UAV;attitude tracking;extremum seeking;feedback gain tuning
spellingShingle GUO Dali
ZHAO Zhongyuan
LUO Zijuan
Attitude tracking control for quadrotor UAVs based on extremum seeking
智能科学与技术学报
quadrotor UAV;attitude tracking;extremum seeking;feedback gain tuning
title Attitude tracking control for quadrotor UAVs based on extremum seeking
title_full Attitude tracking control for quadrotor UAVs based on extremum seeking
title_fullStr Attitude tracking control for quadrotor UAVs based on extremum seeking
title_full_unstemmed Attitude tracking control for quadrotor UAVs based on extremum seeking
title_short Attitude tracking control for quadrotor UAVs based on extremum seeking
title_sort attitude tracking control for quadrotor uavs based on extremum seeking
topic quadrotor UAV;attitude tracking;extremum seeking;feedback gain tuning
url http://www.cjist.com.cn/thesisDetails#10.11959/j.issn.2096-6652.202337
work_keys_str_mv AT guodali attitudetrackingcontrolforquadrotoruavsbasedonextremumseeking
AT zhaozhongyuan attitudetrackingcontrolforquadrotoruavsbasedonextremumseeking
AT luozijuan attitudetrackingcontrolforquadrotoruavsbasedonextremumseeking