Design of EKV Sliding Mode Guidance Law Based on Terminal Angle Limit

NIE  Chuang; SHU  Jiansheng; MENG  Shaofei

doi:10.15892/j.cnki.djzdxb.2015.05.006

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Journal of Projectiles, Rockets, Missiles and Guidance ›› 2015, Vol. 35 ›› Issue (5) : 22-24,29. DOI: 10.15892/j.cnki.djzdxb.2015.05.006

MISSILES AND GUIDANCE TECHNOLOGY

Design of EKV Sliding Mode Guidance Law Based on Terminal Angle Limit

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{{article.zuoZheEn_L}}. {{article.title_en}}[J]. {{journal.qiKanMingCheng_EN}}, 2015, 35(5): 22-24,29 https://doi.org/10.15892/j.cnki.djzdxb.2015.05.006

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Received	Published
2014-10-29	2015-10-20
Issue Date
2025-05-28

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