Research on Adaptive Control Method of Variable-sweep Wing Aircraft Based on Neural Network

LI  Moyin; MA  Zeyuan; ZHOU  Jianping; ZHANG  Yunfei; XIA  Qunli

doi:10.15892/j.cnki.djzdxb.2021.05.015

LI Moyin, MA Zeyuan, ZHOU Jianping, ZHANG Yunfei, XIA Qunli

Journal of Projectiles, Rockets, Missiles and Guidance ›› 2021, Vol. 41 ›› Issue (5) : 73-77.

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Journal of Projectiles, Rockets, Missiles and Guidance ›› 2021, Vol. 41 ›› Issue (5) : 73-77. DOI: 10.15892/j.cnki.djzdxb.2021.05.015

Research on Adaptive Control Method of Variable-sweep Wing Aircraft Based on Neural Network

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{{article.zuoZheEn_L}}. {{article.title_en}}[J]. {{journal.qiKanMingCheng_EN}}, 2021, 41(5): 73-77 https://doi.org/10.15892/j.cnki.djzdxb.2021.05.015

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Received	Published
2020-11-30	2021-10-20
Issue Date
2025-05-30

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