PD Controller with Particle Swarm Optimization for Satellite Attitude Control

Mehmet Fatih Erturk; Chingiz Hajiyev

doi:10.1007/978-3-031-37160-8_11

PD Controller with Particle Swarm Optimization for Satellite Attitude Control

Mehmet Fatih Erturk^*
, Chingiz Hajiyev

^*Corresponding author for this work

Department of Aeronautical Engineering

Istanbul Technical University

Research output: Chapter in Book/Report/Conference proceeding › Chapter › peer-review

1 Citation (Scopus)

Abstract

In this study, a PD controller is used as an attitude controller with using only magnetic actuator. Gain of the PD controller is tuned by a particle swarm optimization to increase the pointing accuracy of an Earth-oriented satellite. While deterministic approach is used, increase of the performance of the satellite controller is observed.

Original language	English
Title of host publication	Sustainable Aviation
Publisher	Springer Nature
Pages	67-73
Number of pages	7
DOIs	https://doi.org/10.1007/978-3-031-37160-8_11
Publication status	Published - 2023

Publication series

Name	Sustainable Aviation
Volume	Part F4677
ISSN (Print)	2730-7778
ISSN (Electronic)	2730-7786

Bibliographical note

Publisher Copyright:
© The Author(s), under exclusive license to Springer Nature Switzerland AG 2023.

Keywords

Attitude control
Gain optimization
PD controller

Access to Document

10.1007/978-3-031-37160-8_11

Cite this

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abstract = "In this study, a PD controller is used as an attitude controller with using only magnetic actuator. Gain of the PD controller is tuned by a particle swarm optimization to increase the pointing accuracy of an Earth-oriented satellite. While deterministic approach is used, increase of the performance of the satellite controller is observed.",

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KW - Gain optimization

KW - PD controller

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PB - Springer Nature

ER -

PD Controller with Particle Swarm Optimization for Satellite Attitude Control

Abstract

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Keywords

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