The Design of Wind Tunnel Based Virtual Flight Testing Control System

CHEN  Xingyang; ZHENG  Kunpeng

doi:10.15892/j.cnki.djzdxb.2013.06.040

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Journal of Projectiles, Rockets, Missiles and Guidance ›› 2013, Vol. 33 ›› Issue (6) : 129-132. DOI: 10.15892/j.cnki.djzdxb.2013.06.040

MISSILES AND GUIDANCE TECHNOLOGY

The Design of Wind Tunnel Based Virtual Flight Testing Control System

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{{article.zuoZheEn_L}}. {{article.title_en}}[J]. {{journal.qiKanMingCheng_EN}}, 2013, 33(6): 129-132 https://doi.org/10.15892/j.cnki.djzdxb.2013.06.040

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Received	Published
2013-01-21	2013-12-20
Issue Date
2025-05-26

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