Fuzzy Adaptive Adjusted Sliding Mold VSC for Designing Missile Attitude Control System

TANG  Yidong; LI  Xiaobing; QIAO  Pengpeng

doi:10.15892/j.cnki.djzdxb.2013.02.036

TANG Yidong, LI Xiaobing, QIAO Pengpeng

Journal of Projectiles, Rockets, Missiles and Guidance ›› 2013, Vol. 33 ›› Issue (2) : 15-18.

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Journal of Projectiles, Rockets, Missiles and Guidance ›› 2013, Vol. 33 ›› Issue (2) : 15-18. DOI: 10.15892/j.cnki.djzdxb.2013.02.036

MISSILES AND GUIDANCE TECHNOLOGY

Fuzzy Adaptive Adjusted Sliding Mold VSC for Designing Missile Attitude Control System

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{{article.zuoZheEn_L}}. {{article.title_en}}[J]. {{journal.qiKanMingCheng_EN}}, 2013, 33(2): 15-18 https://doi.org/10.15892/j.cnki.djzdxb.2013.02.036

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Received	Published
2012-09-24	2013-04-20
Issue Date
2025-05-26

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