A Calculation Method of Aircraft's Rolling Dynamic Derivatives Based on Quasi-steady Assumption

MI  Baigang; ZHAN  Hao; ZHU  Jun

doi:10.15892/j.cnki.djzdxb.2013.03.029

MI Baigang, ZHAN Hao, ZHU Jun

Journal of Projectiles, Rockets, Missiles and Guidance ›› 2013, Vol. 33 ›› Issue (3) : 21-24.

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Journal of Projectiles, Rockets, Missiles and Guidance ›› 2013, Vol. 33 ›› Issue (3) : 21-24. DOI: 10.15892/j.cnki.djzdxb.2013.03.029

MISSILES AND GUIDANCE TECHNOLOGY

A Calculation Method of Aircraft's Rolling Dynamic Derivatives Based on Quasi-steady Assumption

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{{article.zuoZheEn_L}}. {{article.title_en}}[J]. {{journal.qiKanMingCheng_EN}}, 2013, 33(3): 21-24 https://doi.org/10.15892/j.cnki.djzdxb.2013.03.029

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Received	Published
2012-10-18	2013-06-20
Issue Date
2025-05-26

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