Spacecraft Attitude Determination of REQUEST/CKF Integration

XIAO  Zhicai; LI  Haijun; WANG  Zhen

doi:10.15892/j.cnki.djzdxb.2015.06.001

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Journal of Projectiles, Rockets, Missiles and Guidance ›› 2015, Vol. 35 ›› Issue (6) : 1-4,8. DOI: 10.15892/j.cnki.djzdxb.2015.06.001

MISSILES AND GUIDANCE TECHNOLOGY

Spacecraft Attitude Determination of REQUEST/CKF Integration

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{{article.zuoZheEn_L}}. {{article.title_en}}[J]. {{journal.qiKanMingCheng_EN}}, 2015, 35(6): 1-4,8 https://doi.org/10.15892/j.cnki.djzdxb.2015.06.001

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Received	Published
2014-11-05	2015-12-20
Issue Date
2025-05-28

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