Dynamic Inversion Autopilot Design for Loiter Missile Based on Neural Network

DU  Dacheng; LIU  Li; LI  Huaijian; YU  Jianqiao

doi:10.15892/j.cnki.djzdxb.2010.06.036

DU Dacheng, LIU Li, LI Huaijian, YU Jianqiao

Journal of Projectiles, Rockets, Missiles and Guidance ›› 2010, Vol. 30 ›› Issue (6) : 42-45.

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Journal of Projectiles, Rockets, Missiles and Guidance ›› 2010, Vol. 30 ›› Issue (6) : 42-45. DOI: 10.15892/j.cnki.djzdxb.2010.06.036

MISSILES AND GUIDANCE TECHNOLOGY

Dynamic Inversion Autopilot Design for Loiter Missile Based on Neural Network

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{{article.zuoZheEn_L}}. {{article.title_en}}[J]. {{journal.qiKanMingCheng_EN}}, 2010, 30(6): 42-45 https://doi.org/10.15892/j.cnki.djzdxb.2010.06.036

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Received	Published
2010-03-24	2010-12-20
Issue Date
2025-05-28

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