Six Degree-of-freedom Trajectory Model of Plane-symmetry Rolling Missiles Based on Non-spinning Body Coordinate System

GAO  Qingfeng; XIA  Qunli; FANG  Shuzhou; CHEN  Luojing

doi:10.15892/j.cnki.djzdxb.2010.04.038

GAO Qingfeng, XIA Qunli, FANG Shuzhou, CHEN Luojing

Journal of Projectiles, Rockets, Missiles and Guidance ›› 2010, Vol. 30 ›› Issue (4) : 149-152,168.

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Journal of Projectiles, Rockets, Missiles and Guidance ›› 2010, Vol. 30 ›› Issue (4) : 149-152,168. DOI: 10.15892/j.cnki.djzdxb.2010.04.038

BALLISTIC AND AIRDYNAMICS

Six Degree-of-freedom Trajectory Model of Plane-symmetry Rolling Missiles Based on Non-spinning Body Coordinate System

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{{article.zuoZheEn_L}}. {{article.title_en}}[J]. {{journal.qiKanMingCheng_EN}}, 2010, 30(4): 149-152,168 https://doi.org/10.15892/j.cnki.djzdxb.2010.04.038

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Received	Published
2009-09-09	2010-08-20
Issue Date
2025-05-28

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