The Attitude Decoupling Control of the Flying Wing UAVBased on the Differential Geometry Method

QU  Gaomin; LI  Jiguang

doi:10.15892/j.cnki.djzdxb.2018.02.026

QU Gaomin, LI Jiguang

Journal of Projectiles, Rockets, Missiles and Guidance ›› 2018, Vol. 38 ›› Issue (2) : 116-122.

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Journal of Projectiles, Rockets, Missiles and Guidance ›› 2018, Vol. 38 ›› Issue (2) : 116-122. DOI: 10.15892/j.cnki.djzdxb.2018.02.026

The Attitude Decoupling Control of the Flying Wing UAVBased on the Differential Geometry Method

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{{article.zuoZheEn_L}}. {{article.title_en}}[J]. {{journal.qiKanMingCheng_EN}}, 2018, 38(2): 116-122 https://doi.org/10.15892/j.cnki.djzdxb.2018.02.026

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Received	Published
2017-07-30	2018-04-20
Issue Date
2025-05-28

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