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23977

FUZZY LOGIC CONTROLLER TUNNING VIA ADAPTIVE GENETIC ALGORITHM APPLIED TO AIRCRAFT LONGITUDINAL MOTION

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Last updated: 24 Dec 2024

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Abstract

ABSTRACT
Design of an efficient fuzzy logic controller involves the optimization of parameters of fuzzy sets, denormalized gains and proper choice of rule base. There are several techniques reported in recent literature that use genetic algorithms to learn and optimize a fuzzy logic controller. This paper develops methodologies to learn and optimize fuzzy logic controller parameters based on genetic algorithm. The strategies developed have been applied to control integration between LQR and nonlinear Fuzzy PID of F16 aircraft pitch motion control and fuzzy controller developed with the help of iterative learning from operator experience. The results show that Genetic-Fuzzy approaches were able to learn rule base and identify membership function parameters accurately.

DOI

10.21608/asat.2007.23977

Keywords

Intelligent control, Fuzzy Logic, Genetic Algorithm, Linear quadratic regulator

Authors

First Name

Ahmed

Last Name

Momtaz

MiddleName

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Affiliation

PHD Candidate, School of astronautics, Beihang University, Beijing, China.

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City

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Orcid

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First Name

Han

Last Name

Chao

MiddleName

-

Affiliation

Professor, School of astronautics, Beihang University, Beijing, China.

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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

13

Print ISSN

2090-0678

Online ISSN

2636-364X

Link

https://asat.journals.ekb.eg/article_23977.html

Detail API

https://asat.journals.ekb.eg/service?article_code=23977

Order

58

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

FUZZY LOGIC CONTROLLER TUNNING VIA ADAPTIVE GENETIC ALGORITHM APPLIED TO AIRCRAFT LONGITUDINAL MOTION

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Article

Created At

22 Jan 2023