Estimation of the Attitude of a Rolling Missile Based on Square Root-unscented Kalman Filter

ZOU  Yimin

doi:10.15892/j.cnki.djzdxb.2010.04.035

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Journal of Projectiles, Rockets, Missiles and Guidance ›› 2010, Vol. 30 ›› Issue (4) : 41-44. DOI: 10.15892/j.cnki.djzdxb.2010.04.035

MIISSILES AND GUIDANCE TECHNOLOGY

Estimation of the Attitude of a Rolling Missile Based on Square Root-unscented Kalman Filter

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{{article.zuoZheEn_L}}. {{article.title_en}}[J]. {{journal.qiKanMingCheng_EN}}, 2010, 30(4): 41-44 https://doi.org/10.15892/j.cnki.djzdxb.2010.04.035

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Received	Published
2009-10-14	2010-08-20
Issue Date
2025-05-28

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