Autopilot Design Based on Fuzzy Logic for a Dual-controlled Missile

ZHAO  Yanhui; ZHANG  Gongping; YANG  Yurong

doi:10.15892/j.cnki.djzdxb.2014.03.037

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Journal of Projectiles, Rockets, Missiles and Guidance ›› 2014, Vol. 34 ›› Issue (3) : 33-36. DOI: 10.15892/j.cnki.djzdxb.2014.03.037

MISSILES AND GUIDANCE TECHNOLOGY

Autopilot Design Based on Fuzzy Logic for a Dual-controlled Missile

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{{article.zuoZheEn_L}}. {{article.title_en}}[J]. {{journal.qiKanMingCheng_EN}}, 2014, 34(3): 33-36 https://doi.org/10.15892/j.cnki.djzdxb.2014.03.037

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Received	Published
2013-07-02	2014-06-20
Issue Date
2025-05-30

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