Optimized Design on Vibration-isolation of Inertial Navigation by Using Finite Element Method

CHENG  Wenjuan; BAI  Zhen; HE  Ning

doi:10.15892/j.cnki.djzdxb.2014.06.012

CHENG Wenjuan, BAI Zhen, HE Ning

Journal of Projectiles, Rockets, Missiles and Guidance ›› 2014, Vol. 34 ›› Issue (6) : 47-50.

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Journal of Projectiles, Rockets, Missiles and Guidance ›› 2014, Vol. 34 ›› Issue (6) : 47-50. DOI: 10.15892/j.cnki.djzdxb.2014.06.012

MISSILES AND GUIDANCE TECHNOLOGY

Optimized Design on Vibration-isolation of Inertial Navigation by Using Finite Element Method

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{{article.zuoZheEn_L}}. {{article.title_en}}[J]. {{journal.qiKanMingCheng_EN}}, 2014, 34(6): 47-50 https://doi.org/10.15892/j.cnki.djzdxb.2014.06.012

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Received	Published
2014-02-03	2014-12-20
Issue Date
2025-05-30

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