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143250

Momentum Biased Satellite Attitude Stablization Using PD Controller with Fuzzy Gain Adjustment.

Article

Last updated: 04 Jan 2025

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Subjects

-

Tags

Mechanical Power Engineering

Abstract

 Momentum biased satellites are dual spin satellites in which constant angular momentum is provided by a momentum wheel. The momentum bias is not sufficient to stabilize completely the momentum axis in space. Active control is used to assure accurate altitude stabilization. Control of the roil and yaw angles with and without yaw measurement will be analyzed. Control engineers prefer not to use angular rate sensors except for very special tasks and for short periods. The rate of Euler angles will be obtained by differentiation, with the adequate noise filters. Fuzzy gain adjustment is used for the case of momentum biased satellites without yaw measurement in order to minimize error. The gain, output scaling factor, of the controller is adjusted on line according to the current states of the controlled process. 

DOI

10.21608/bfemu.2021.143250

Keywords

Momentum Biased Satellites, Stabilization, Fuzzy control, Self tuning

Authors

First Name

G.

Last Name

El-Bayoumi

MiddleName

M.

Affiliation

Faculty of Engineering., Cairo University., Giza., Egypt.

Email

-

City

Giza

Orcid

-

Volume

27

Article Issue

4

Related Issue

21026

Issue Date

2002-12-01

Receive Date

2002-09-26

Publish Date

2021-01-25

Page Start

23

Page End

40

Print ISSN

1110-0923

Online ISSN

2735-4202

Article File

BFEMU_Volume 27_Issue 4_Pages 23-40.pdf

PDF . 346.7kB

Link

https://bfemu.journals.ekb.eg/article_143250.html

Detail API

https://bfemu.journals.ekb.eg/service?article_code=143250

Order

12

Type

Research Studies

Type Code

1,205

Publication Type

Journal

Publication Title

MEJ. Mansoura Engineering Journal

Publication Link

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

MainTitle

Momentum Biased Satellite Attitude Stablization Using PD Controller with Fuzzy Gain Adjustment.

Details

Type

Article

Created At

22 Jan 2023