Decoupling Control Method Based on Incremental Nonlinear Dynamic Inversion for Missiles

CHEN Xingyang; ZHAO Xia; ZHOU Xiaozhi; LI Liang

doi:10.15892/j.cnki.djzdxb.2024.02.012

CHEN Xingyang, ZHAO Xia, ZHOU Xiaozhi, LI Liang

Journal of Projectiles, Rockets, Missiles and Guidance ›› 2024, Vol. 44 ›› Issue (2) : 76-81.

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Journal of Projectiles, Rockets, Missiles and Guidance ›› 2024, Vol. 44 ›› Issue (2) : 76-81. DOI: 10.15892/j.cnki.djzdxb.2024.02.012

Decoupling Control Method Based on Incremental Nonlinear Dynamic Inversion for Missiles

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{{article.zuoZheEn_L}}. {{article.title_en}}[J]. {{journal.qiKanMingCheng_EN}}, 2024, 44(2): 76-81 https://doi.org/10.15892/j.cnki.djzdxb.2024.02.012

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Received	Published
2023-09-25	2024-04-20
Issue Date
2024-12-28

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