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Adaptive Fuzzy Sliding-Mode Tracking Control for a VTOL Aircraft System Under Predefined Performance

Minglong Zhou Xiongfeng Deng

无人系统（英文）2025，Vol.13Issue(3)：789-799,11.

无人系统（英文）2025，Vol.13Issue(3)：789-799,11.DOI:10.1142/S2301385025500487

Adaptive Fuzzy Sliding-Mode Tracking Control for a VTOL Aircraft System Under Predefined Performance

Minglong Zhou ¹Xiongfeng Deng²

作者信息

1. College of Electrical Engineering,Anhui Technical College of Mechanical and Electrical Engineering,Wuhu Anhui 241000,P.R.China
2. Key Laboratory of Electric Drive and Control of Anhui Higher Education Institutes,Anhui Polytechnic University,Wuhu,Anhui 241000,P.R.China
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摘要

关键词

Fuzzy logic system/sliding-mode control/VTOL aircraft/predefined performance/adaptive control

Key words

Fuzzy logic system/sliding-mode control/VTOL aircraft/predefined performance/adaptive control

引用本文复制引用

Minglong Zhou,Xiongfeng Deng..Adaptive Fuzzy Sliding-Mode Tracking Control for a VTOL Aircraft System Under Predefined Performance[J].无人系统（英文）,2025,13(3):789-799,11.

基金项目

This work was partially supported by the Open Fund of the National Key Laboratory of Helicopter Aeromechanics under the Grant 2024-ZSJ-LB-02-04,and the Natural Science Re-search of Colleges and Universities of Anhui Province under the Grants 2023AH050908 and 2023AH052698. （）

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