Design of UAV Attitude Controller Based on Fuzzy PID

CHEN  Peng; DUAN  Fengyang; ZHANG  Qingjie; ZHENG  Zhicheng; XIAO  Wei

doi:10.15892/j.cnki.djzdxb.2015.01.003

CHEN Peng, DUAN Fengyang, ZHANG Qingjie, ZHENG Zhicheng, XIAO Wei

Journal of Projectiles, Rockets, Missiles and Guidance ›› 2015, Vol. 35 ›› Issue (1) : 9-11,18.

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Journal of Projectiles, Rockets, Missiles and Guidance ›› 2015, Vol. 35 ›› Issue (1) : 9-11,18. DOI: 10.15892/j.cnki.djzdxb.2015.01.003

MISSILES AND GUIDANCE TECHNOLOGY

Design of UAV Attitude Controller Based on Fuzzy PID

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{{article.zuoZheEn_L}}. {{article.title_en}}[J]. {{journal.qiKanMingCheng_EN}}, 2015, 35(1): 9-11,18 https://doi.org/10.15892/j.cnki.djzdxb.2015.01.003

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Received	Published
2014-02-10	2015-02-20
Issue Date
2025-05-26

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