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26564

ADAPTIVE CONTROL OF LONGITUDINAL FLIGHT OF AIRCRAFT SYSTEM

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Last updated: 04 Jan 2025

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Abstract

This Paper present two proposals for adaptive control of supersonic aircraft. Inthe first proposal, the aircraft complete transfer function is controlled to behave according to a second order chosen model, while in the second proposal the inner loop of the aircraft transfer function is controlled to behave according to a first order model. A modified gradient technique for a model reference adaptive control system with less order model is employed in the two proposals. Analog computer simulation resuits are presented and discussed .

DOI

10.21608/asat.1985.26564

Authors

First Name

A.

Last Name

Azab

MiddleName

A.

Affiliation

Visiting professor at Aero. Eng. Dept. Iowa State University, Ames, Iowa, 50011 . Originally With Military Technical College, Cairo, Egypt .

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Volume

1

Article Issue

A.S.A.T. CONFERENCE 14-16 May 1985 r CAIRO

Related Issue

4758

Issue Date

1985-05-01

Receive Date

2019-02-05

Publish Date

1985-05-01

Page Start

873

Page End

895

Print ISSN

2090-0678

Online ISSN

2636-364X

Article File

ASAT_Volume 1_Issue A.S.A.T. CONFERENCE 14-16 May 1985 r CAIRO_Pages 873-895.pdf

PDF . 3.9MB

Link

https://asat.journals.ekb.eg/article_26564.html

Detail API

https://asat.journals.ekb.eg/service?article_code=26564

Order

73

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

ADAPTIVE CONTROL OF LONGITUDINAL FLIGHT OF AIRCRAFT SYSTEM

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Article

Created At

22 Jan 2023