High Altitude Air Defense with Intelligent Fuzzy Terminal Guidance Law by Taking Turning Rate and Radome Error Slope into Consideration

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Title:	High Altitude Air Defense with Intelligent Fuzzy Terminal Guidance Law by Taking Turning Rate and Radome Error Slope into Consideration
Authors:	林君明 Lin, Jium-Ming
Contributors:	通訊工程學系 Communication Engineering
Keywords:	fuzzy guidance law;proportion navigation;turning rate time constant;radome error slope;miss distance
Date:	2011
Issue Date:	2014-06-27 02:02:15 (UTC+8)
Abstract:	This research provides a missile PD-type as well as PID-type fuzzy terminal guidance laws design for high altitude air defense. Both the missile turning rate time constant and radome slope error are taken into consideration. Comparisons with the tradition
Appears in Collections:	[Department of Communication Engineering] Seminar papers

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