The Design of Trajectory Correction Actuator Based on Fuze Nose Cone Swing

QIN  Huawei; WANG  Hua

doi:10.15892/j.cnki.djzdxb.2013.03.043

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Journal of Projectiles, Rockets, Missiles and Guidance ›› 2013, Vol. 33 ›› Issue (3) : 87-90,101. DOI: 10.15892/j.cnki.djzdxb.2013.03.043

PROJECTILES TECHNOLOGY

The Design of Trajectory Correction Actuator Based on Fuze Nose Cone Swing

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{{article.zuoZheEn_L}}. {{article.title_en}}[J]. {{journal.qiKanMingCheng_EN}}, 2013, 33(3): 87-90,101 https://doi.org/10.15892/j.cnki.djzdxb.2013.03.043

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Received	Published
2012-08-23	2013-06-20
Issue Date
2025-05-26

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