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23982

Development of Fuzzy Logic Controller to Enhance the Performance of a HILS for a Homing Guided Missile

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Last updated: 04 Jan 2025

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Abstract

This paper investigates the application of fuzzy logic for the development of guidance commands for homing missiles. Fuzzy logic approximation of the well-known proportional navigation guidance law is discussed to enhance the interception of targets performing uncertain maneuvers. Fuzzy logic guidance law development employs triangular membership functions. Simulation results using a HILS system are given.

DOI

10.21608/asat.2007.23982

Keywords

Fuzzy Logic controller, Hardware in the loop

Authors

First Name

Elhalwagy

Last Name

Z.

MiddleName

Y.

Affiliation

Dr. , Dpt. of Radar And Guidance, Military Technical Collage , Cairo, Egypt.

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First Name

Abdelhady

Last Name

M.

MiddleName

A.

Affiliation

Eng. , Dpt. of Radar And Guidance, Military Technical Collage , Cairo, Egypt.

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City

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Orcid

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First Name

Fahmy

Last Name

E.

MiddleName

A.

Affiliation

Professor , Dpt. of Radar And Guidance, Military Technical Collage , Cairo, Egypt.

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Volume

12

Article Issue

ASAT Conference, 29-31 May 2007

Related Issue

4431

Issue Date

2007-05-01

Receive Date

2019-01-09

Publish Date

2007-05-01

Page Start

1

Page End

12

Print ISSN

2090-0678

Online ISSN

2636-364X

Article File

ASAT_Volume 12_Issue ASAT Conference, 29-31 May 2007_Pages 1-12.pdf

PDF . 712.8kB

Link

https://asat.journals.ekb.eg/article_23982.html

Detail API

https://asat.journals.ekb.eg/service?article_code=23982

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62

Type

Original Article

Type Code

737

Publication Type

Journal

Publication Title

International Conference on Aerospace Sciences and Aviation Technology

Publication Link

https://asat.journals.ekb.eg/

MainTitle

Development of Fuzzy Logic Controller to Enhance the Performance of a HILS for a Homing Guided Missile

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Article

Created At

22 Jan 2023