Design of Multi Missile Formation Flight Controller Based on Sliding Mode Theory

XU Zihe; MING Chao; BAI Zhiheng; GENG Xuelong; FENG Tong

doi:10.15892/j.cnki.djzdxb.2025.04.008

XU Zihe, MING Chao, BAI Zhiheng, GENG Xuelong, FENG Tong

Journal of Projectiles, Rockets, Missiles and Guidance ›› 2025, Vol. 45 ›› Issue (4) : 510-515.

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Journal of Projectiles, Rockets, Missiles and Guidance ›› 2025, Vol. 45 ›› Issue (4) : 510-515. DOI: 10.15892/j.cnki.djzdxb.2025.04.008

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Design of Multi Missile Formation Flight Controller Based on Sliding Mode Theory

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{{article.zuoZheEn_L}}. {{article.title_en}}[J]. {{journal.qiKanMingCheng_EN}}, 2025, 45(4): 510-515 https://doi.org/10.15892/j.cnki.djzdxb.2025.04.008

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Received	Published
2024-12-13	2025-08-20
Issue Date
2025-09-22

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