Design of an Angle of Attack Control Law for Hypersonic Cruise Vehicle Based on Adaptive Sliding Mode Control

XIONG  Ke; XIA  Zhixun; GUO  Zhenyun

doi:10.15892/j.cnki.djzdxb.2010.06.070

XIONG Ke, XIA Zhixun, GUO Zhenyun

Journal of Projectiles, Rockets, Missiles and Guidance ›› 2010, Vol. 30 ›› Issue (6) : 35-38.

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Journal of Projectiles, Rockets, Missiles and Guidance ›› 2010, Vol. 30 ›› Issue (6) : 35-38. DOI: 10.15892/j.cnki.djzdxb.2010.06.070

MISSILES AND GUIDANCE TECHNOLOGY

Design of an Angle of Attack Control Law for Hypersonic Cruise Vehicle Based on Adaptive Sliding Mode Control

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{{article.zuoZheEn_L}}. {{article.title_en}}[J]. {{journal.qiKanMingCheng_EN}}, 2010, 30(6): 35-38 https://doi.org/10.15892/j.cnki.djzdxb.2010.06.070

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Received	Published
2010-04-20	2010-12-20
Issue Date
2025-05-28

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