Missile/Rocket Flight Attitude Test Method Based on Magnetometer and Gyroscope

CUI  Min; MA  Tiehua; DUAN  Jingjing; FAN  Jinbiao

doi:10.15892/j.cnki.djzdxb.2010.06.044

CUI Min, MA Tiehua, DUAN Jingjing, FAN Jinbiao

Journal of Projectiles, Rockets, Missiles and Guidance ›› 2010, Vol. 30 ›› Issue (6) : 85-87.

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Journal of Projectiles, Rockets, Missiles and Guidance ›› 2010, Vol. 30 ›› Issue (6) : 85-87. DOI: 10.15892/j.cnki.djzdxb.2010.06.044

MISSILES AND GUIDANCE TECHNOLOGY

Missile/Rocket Flight Attitude Test Method Based on Magnetometer and Gyroscope

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{{article.zuoZheEn_L}}. {{article.title_en}}[J]. {{journal.qiKanMingCheng_EN}}, 2010, 30(6): 85-87 https://doi.org/10.15892/j.cnki.djzdxb.2010.06.044

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Received	Published
2010-01-04	2010-12-20
Issue Date
2025-05-28

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