Missile Configuration Parameters Design Based on Multidisciplinary Design Optimization

ZHOU  Jian; ZHOU  Yuhong; QIANG  Jinhui; WANG  Zhuping

doi:10.15892/j.cnki.djzdxb.2010.04.042

ZHOU Jian, ZHOU Yuhong, QIANG Jinhui, WANG Zhuping

Journal of Projectiles, Rockets, Missiles and Guidance ›› 2010, Vol. 30 ›› Issue (4) : 19-22.

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Journal of Projectiles, Rockets, Missiles and Guidance ›› 2010, Vol. 30 ›› Issue (4) : 19-22. DOI: 10.15892/j.cnki.djzdxb.2010.04.042

MIISSILES AND GUIDANCE TECHNOLOGY

Missile Configuration Parameters Design Based on Multidisciplinary Design Optimization

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{{article.zuoZheEn_L}}. {{article.title_en}}[J]. {{journal.qiKanMingCheng_EN}}, 2010, 30(4): 19-22 https://doi.org/10.15892/j.cnki.djzdxb.2010.04.042

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Received	Published
2009-10-20	2010-08-20
Issue Date
2025-05-28

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