Beta
170549

Self Adjusting Digital Controller for Aircraft Systems.

Article

Last updated: 22 Jan 2023

Subjects

-

Tags

Electrical Engineering

Abstract

The paper describes an algorithm for designing self adjusting optimal controller for digital aircraft control systems to cope with the variation of the aircraft parameters under different flight conditions. The aircraft parameters which depend on the flight condition are continuously measured. A deadband zone around each of the parameters oa presetting flight condition is initiated. Any deviation from these bands will individually perturb the controller reference for obtaining sensitivity functions. These sensitivity functions will be used to adjust the feedback parameters of the aircraft control system. The proposed technique is suitable for implementation on real world control systems. The design of the proposed control represents an extension for that concepts included in [1]. 
 

DOI

10.21608/bfemu.2021.170549

Authors

First Name

A.

Last Name

Abd El-Gawad

MiddleName

O.

Affiliation

Assistant professor of Electrical Power Engineering Department, Faculty of Engineering, Mansoura University, Mansoura, Egypt.

Email

-

City

Mansoura

Orcid

-

Volume

15

Article Issue

1

Related Issue

24850

Issue Date

1990-06-01

Receive Date

1990-04-18

Publish Date

2021-05-18

Page Start

14

Page End

22

Print ISSN

1110-0923

Online ISSN

2735-4202

Link

https://bfemu.journals.ekb.eg/article_170549.html

Detail API

https://bfemu.journals.ekb.eg/service?article_code=170549

Order

6

Type

Research Studies

Type Code

1,205

Publication Type

Journal

Publication Title

MEJ. Mansoura Engineering Journal

Publication Link

https://bfemu.journals.ekb.eg/

MainTitle

-

Details

Type

Article

Created At

22 Jan 2023