The Research on Pulse Parameter Optimization of Terminal Trajectory Correction Projectile Based on Orthogonal Experimental Design Method

CAO  Yingjun; FENG  Wubin; BI  Xiaomeng; JI  Xiaogang

doi:10.15892/j.cnki.djzdxb.2012.06.048

CAO Yingjun, FENG Wubin, BI Xiaomeng, JI Xiaogang

Journal of Projectiles, Rockets, Missiles and Guidance ›› 2012, Vol. 32 ›› Issue (6) : 136-139.

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Journal of Projectiles, Rockets, Missiles and Guidance ›› 2012, Vol. 32 ›› Issue (6) : 136-139. DOI: 10.15892/j.cnki.djzdxb.2012.06.048

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The Research on Pulse Parameter Optimization of Terminal Trajectory Correction Projectile Based on Orthogonal Experimental Design Method

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{{article.zuoZheEn_L}}. {{article.title_en}}[J]. {{journal.qiKanMingCheng_EN}}, 2012, 32(6): 136-139 https://doi.org/10.15892/j.cnki.djzdxb.2012.06.048

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Received	Published
2012-03-03	2012-12-20
Issue Date
2025-05-29

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