Flight Control System Design Via Nonlinear Robust Dynamic Inversion

SUN  Xiaoxu; SHAN  Jiayuan

doi:10.15892/j.cnki.djzdxb.2014.05.011

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Journal of Projectiles, Rockets, Missiles and Guidance ›› 2014, Vol. 34 ›› Issue (5) : 41-45. DOI: 10.15892/j.cnki.djzdxb.2014.05.011

MISSILES AND GUIDANCE TECHNOLOGY

Flight Control System Design Via Nonlinear Robust Dynamic Inversion

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{{article.zuoZheEn_L}}. {{article.title_en}}[J]. {{journal.qiKanMingCheng_EN}}, 2014, 34(5): 41-45 https://doi.org/10.15892/j.cnki.djzdxb.2014.05.011

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Received	Published
2013-12-04	2014-10-20
Issue Date
2025-05-30

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