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64936

Fault Detection and Avoidance for Spacecraft Failure using PSO Algorithm

Article

Last updated: 04 Jan 2025

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Abstract

Fault detection algorithm design of satellite inflight control is important for most remote sensing satellites. The responsibility of a satellite attitude control system always keeps the satellite in a stable mode. A satellite control mode contains standby, imaging and detumbling modes. Before we start imaging, we used to prepare an attitude control system to change satellite angles according to payload camera planning schedule to shoot a specific area of interest. After imaging is complete, the attitude control changes satellite angles back to nadir (zero tilting angels). Some control problems may cause failures which put the satellite in a detumbling mode due to accumulated torque on reaction wheel of the satellite. Artificial intelligent design algorithm of particle swarm optimization (PSO) is proposed to control the satellite in real-time mode, which decreases the angular velocity received from the satellite. This approach calculates the difference between the real-time measurement and the designed angular velocity (∆θ) within the satellite communication session time. The Matlab customization function implements PSO controller. The mathematical model of satellite attitude control system has been designed according to the satellite dynamics and kinematics laws. The approached mathematical model is implemented using Simulink Matlab tools.

DOI

10.21608/mjeer.2019.64936

Keywords

Fault diagnosis algorithm, particle swarm optimization (PSO), satellite control, and Euler’s moment equations

Authors

First Name

Yassin

Last Name

Yassin

MiddleName

M.

Affiliation

Ground Station, Mission Control Center Flight Director National Authority for Remote Sensing and Space Science (NARSS) Cairo, Egypt

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First Name

Wael

Last Name

Murtada

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Affiliation

On-Board Computer & Space software, PH.D National Authority for Remote Sensing and Space Science (NARSS) Cairo, Egypt

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Orcid

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First Name

Ahmed

Last Name

El Mahallawy

MiddleName

-

Affiliation

department of Computer Science and Engineering, Ph.D Monoufia University Monoufia, Egypt

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Volume

28

Article Issue

ICEEM2019-Special Issue

Related Issue

9704

Issue Date

2019-12-01

Receive Date

2019-12-12

Publish Date

2019-12-01

Page Start

300

Page End

305

Print ISSN

1687-1189

Online ISSN

2682-3535

Link

https://mjeer.journals.ekb.eg/article_64936.html

Detail API

https://mjeer.journals.ekb.eg/service?article_code=64936

Order

9

Type

Original Article

Type Code

1,088

Publication Type

Journal

Publication Title

Menoufia Journal of Electronic Engineering Research

Publication Link

https://mjeer.journals.ekb.eg/

MainTitle

Fault Detection and Avoidance for Spacecraft Failure using PSO Algorithm

Details

Type

Article

Created At

22 Jan 2023