Optimal Guidance Law with Terminal Angular Constraint Use in Air-to-ground Missile

CHEN  Yun; CHANG  Yan; MIAO  Haochun; YAN  Xianjun

doi:10.15892/j.cnki.djzdxb.2018.05.032

CHEN Yun, CHANG Yan, MIAO Haochun, YAN Xianjun

Journal of Projectiles, Rockets, Missiles and Guidance ›› 2018, Vol. 38 ›› Issue (5) : 141-144.

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Journal of Projectiles, Rockets, Missiles and Guidance ›› 2018, Vol. 38 ›› Issue (5) : 141-144. DOI: 10.15892/j.cnki.djzdxb.2018.05.032

Optimal Guidance Law with Terminal Angular Constraint Use in Air-to-ground Missile

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{{article.zuoZheEn_L}}. {{article.title_en}}[J]. {{journal.qiKanMingCheng_EN}}, 2018, 38(5): 141-144 https://doi.org/10.15892/j.cnki.djzdxb.2018.05.032

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Received	Published
2017-04-20	2018-10-20
Issue Date
2025-05-29

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