STUDY AND IMPLEMENTATION OF FUZZY LOGIC CONTROL SYSTEM FOR GUIDED MISSILES

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DC Field	Value	Language
dc.contributor.author	Narwal, Amit	-
dc.date.accessioned	2025-07-02T13:32:00Z	-
dc.date.available	2025-07-02T13:32:00Z	-
dc.date.issued	2013-06	-
dc.identifier.uri	http://localhost:8081/jspui/handle/123456789/17554	-
dc.description.abstract	In this dissertation the guidance law strategy is made for supposed or assumed missile target dynamics. The law has two operational parts such as midcourse guidance law and terminal guidance law. The fuzzy rules are made separately for both. By using different types of membership functions and their combinations, the simulation has been done for checking which membership function gives the desired performance.	en_US
dc.description.sponsorship	INDIAN INSTITUTE OF TECHNOLOGY ROORKEE	en_US
dc.language.iso	en	en_US
dc.publisher	I I T ROORKEE	en_US
dc.subject	Guidance Law	en_US
dc.subject	Law	en_US
dc.subject	Membership	en_US
dc.subject	Their Combinations	en_US
dc.title	STUDY AND IMPLEMENTATION OF FUZZY LOGIC CONTROL SYSTEM FOR GUIDED MISSILES	en_US
dc.type	Other	en_US
Appears in Collections:	MASTERS' THESES (Electrical Engg)

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