Design of a Missile’s Attitude Tracking Controller Based on H∞ Robust Output Feedback

GU Quan-ying;SONG Jian-mei

Acta Armamentarii ›› 2007, Vol. 28 ›› Issue (6) : 682-685. DOI: 10.3969/j.issn.1000-1093.2007.06.009
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Design of a Missile’s Attitude Tracking Controller Based on H∞ Robust Output Feedback

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{{article.zuoZheEn_L}}. {{article.title_en}}. {{journal.qiKanMingCheng_EN}}. 2007, 28(6): 682-685 https://doi.org/10.3969/j.issn.1000-1093.2007.06.009

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