Optimal Terminal Guidance Law Design Based on NTSM and Adaptive Control

LV  Yongjia; ZHANG  Hexin; WU  Yubin; FAN  Jinsuo; LI  Zhengwen

doi:10.15892/j.cnki.djzdxb.2012.01.041

LV Yongjia, ZHANG Hexin, WU Yubin, FAN Jinsuo, LI Zhengwen

Journal of Projectiles, Rockets, Missiles and Guidance ›› 2012, Vol. 32 ›› Issue (1) : 69-72,88.

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Journal of Projectiles, Rockets, Missiles and Guidance ›› 2012, Vol. 32 ›› Issue (1) : 69-72,88. DOI: 10.15892/j.cnki.djzdxb.2012.01.041

MISSILES AND GUIDANCE TECHNOLOGY

Optimal Terminal Guidance Law Design Based on NTSM and Adaptive Control

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{{article.zuoZheEn_L}}. {{article.title_en}}[J]. {{journal.qiKanMingCheng_EN}}, 2012, 32(1): 69-72,88 https://doi.org/10.15892/j.cnki.djzdxb.2012.01.041

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Received	Published
2010-11-23	2012-02-20
Issue Date
2025-05-29

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