Missile Guidance Law Design via μ-Synthesis
Author:
Publisher
Japan Society for Aeronautical and Space Sciences
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://www.jstage.jst.go.jp/article/tjsass/45/148/45_148_102/_pdf
Reference14 articles.
1. Missile guidance design tradeoffs for high-altitude air defense
2. Proportional navigation and weaving targets
3. Root-mean-square miss distance of proportional navigation missile against sinusoidal target
Cited by 3 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献
1. Design of an H∞ Gain-Scheduled Guidance Scheme for a Guided Projectile;Journal of Guidance, Control, and Dynamics;2019-11
2. Design of an H ∞Gain-Scheduled Guidance Scheme for a Guided Projectile;AIAA Scitech 2019 Forum;2019-01-06
3. Design of a Compensator for Proportional Navigation with .MU.-Synthesis;JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES;2005
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