Development of Satellite Attitude Controller with TRIAD and Particle Swarm Optimization Using Only Magnetic Actuators

Mehmet Fatih Erturk; Chingiz Hajiyev

doi:10.1109/PCI60110.2023.10325920

Development of Satellite Attitude Controller with TRIAD and Particle Swarm Optimization Using Only Magnetic Actuators

Mehmet Fatih Erturk^*, Chingiz Hajiyev

^*Corresponding author for this work

Department of Aeronautical Engineering

Turkish Aerospace Industries

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

1 Citation (Scopus)

Abstract

In this paper, a basic CubeSat model is tried to be controlled with optimizing gain parameters of linear quadratic regulator. Noisy sensor measurements are used to determine attitude by using TRIAD. To reduce the effects of noise in optimization process, a two-step optimization approach is implemented. As a result of this approach, particle swarm optimization achieved to tune gain parameters of the controller.

Original language	English
Title of host publication	2023 5th International Conference on Problems of Cybernetics and Informatics, PCI 2023
Publisher	Institute of Electrical and Electronics Engineers Inc.
ISBN (Electronic)	9798350319064
DOIs	https://doi.org/10.1109/PCI60110.2023.10325920
Publication status	Published - 2023
Event	5th International Conference on Problems of Cybernetics and Informatics, PCI 2023 - Baku, Azerbaijan Duration: 28 Aug 2023 → 30 Aug 2023

Publication series

Name	2023 5th International Conference on Problems of Cybernetics and Informatics, PCI 2023

Conference

Conference	5th International Conference on Problems of Cybernetics and Informatics, PCI 2023
Country/Territory	Azerbaijan
City	Baku
Period	28/08/23 → 30/08/23

Bibliographical note

Publisher Copyright:
© 2023 IEEE.

Keywords

attitude controller
CubeSat
linear quadratic regulator
magnetic control
magnetorquer
satellite

Access to Document

10.1109/PCI60110.2023.10325920

Cite this

Erturk, M. F., & Hajiyev, C. (2023). Development of Satellite Attitude Controller with TRIAD and Particle Swarm Optimization Using Only Magnetic Actuators. In 2023 5th International Conference on Problems of Cybernetics and Informatics, PCI 2023 (2023 5th International Conference on Problems of Cybernetics and Informatics, PCI 2023). Institute of Electrical and Electronics Engineers Inc.. https://doi.org/10.1109/PCI60110.2023.10325920

Erturk, Mehmet Fatih ; Hajiyev, Chingiz. / Development of Satellite Attitude Controller with TRIAD and Particle Swarm Optimization Using Only Magnetic Actuators. 2023 5th International Conference on Problems of Cybernetics and Informatics, PCI 2023. Institute of Electrical and Electronics Engineers Inc., 2023. (2023 5th International Conference on Problems of Cybernetics and Informatics, PCI 2023).

@inproceedings{8c2407f291c14fdcaa3b22978939ed8e,

title = "Development of Satellite Attitude Controller with TRIAD and Particle Swarm Optimization Using Only Magnetic Actuators",

abstract = "In this paper, a basic CubeSat model is tried to be controlled with optimizing gain parameters of linear quadratic regulator. Noisy sensor measurements are used to determine attitude by using TRIAD. To reduce the effects of noise in optimization process, a two-step optimization approach is implemented. As a result of this approach, particle swarm optimization achieved to tune gain parameters of the controller.",

keywords = "attitude controller, CubeSat, linear quadratic regulator, magnetic control, magnetorquer, satellite",

author = "Erturk, {Mehmet Fatih} and Chingiz Hajiyev",

note = "Publisher Copyright: {\textcopyright} 2023 IEEE.; 5th International Conference on Problems of Cybernetics and Informatics, PCI 2023 ; Conference date: 28-08-2023 Through 30-08-2023",

year = "2023",

doi = "10.1109/PCI60110.2023.10325920",

language = "English",

series = "2023 5th International Conference on Problems of Cybernetics and Informatics, PCI 2023",

publisher = "Institute of Electrical and Electronics Engineers Inc.",

booktitle = "2023 5th International Conference on Problems of Cybernetics and Informatics, PCI 2023",

address = "United States",

}

Erturk, MF & Hajiyev, C 2023, Development of Satellite Attitude Controller with TRIAD and Particle Swarm Optimization Using Only Magnetic Actuators. in 2023 5th International Conference on Problems of Cybernetics and Informatics, PCI 2023. 2023 5th International Conference on Problems of Cybernetics and Informatics, PCI 2023, Institute of Electrical and Electronics Engineers Inc., 5th International Conference on Problems of Cybernetics and Informatics, PCI 2023, Baku, Azerbaijan, 28/08/23. https://doi.org/10.1109/PCI60110.2023.10325920

Development of Satellite Attitude Controller with TRIAD and Particle Swarm Optimization Using Only Magnetic Actuators. / Erturk, Mehmet Fatih; Hajiyev, Chingiz.
2023 5th International Conference on Problems of Cybernetics and Informatics, PCI 2023. Institute of Electrical and Electronics Engineers Inc., 2023. (2023 5th International Conference on Problems of Cybernetics and Informatics, PCI 2023).

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

TY - GEN

T1 - Development of Satellite Attitude Controller with TRIAD and Particle Swarm Optimization Using Only Magnetic Actuators

AU - Erturk, Mehmet Fatih

AU - Hajiyev, Chingiz

PY - 2023

Y1 - 2023

N2 - In this paper, a basic CubeSat model is tried to be controlled with optimizing gain parameters of linear quadratic regulator. Noisy sensor measurements are used to determine attitude by using TRIAD. To reduce the effects of noise in optimization process, a two-step optimization approach is implemented. As a result of this approach, particle swarm optimization achieved to tune gain parameters of the controller.

AB - In this paper, a basic CubeSat model is tried to be controlled with optimizing gain parameters of linear quadratic regulator. Noisy sensor measurements are used to determine attitude by using TRIAD. To reduce the effects of noise in optimization process, a two-step optimization approach is implemented. As a result of this approach, particle swarm optimization achieved to tune gain parameters of the controller.

KW - attitude controller

KW - CubeSat

KW - linear quadratic regulator

KW - magnetic control

KW - magnetorquer

KW - satellite

UR - http://www.scopus.com/inward/record.url?scp=85179890193&partnerID=8YFLogxK

U2 - 10.1109/PCI60110.2023.10325920

DO - 10.1109/PCI60110.2023.10325920

M3 - Conference contribution

AN - SCOPUS:85179890193

T3 - 2023 5th International Conference on Problems of Cybernetics and Informatics, PCI 2023

BT - 2023 5th International Conference on Problems of Cybernetics and Informatics, PCI 2023

PB - Institute of Electrical and Electronics Engineers Inc.

T2 - 5th International Conference on Problems of Cybernetics and Informatics, PCI 2023

Y2 - 28 August 2023 through 30 August 2023

ER -

Erturk MF, Hajiyev C. Development of Satellite Attitude Controller with TRIAD and Particle Swarm Optimization Using Only Magnetic Actuators. In 2023 5th International Conference on Problems of Cybernetics and Informatics, PCI 2023. Institute of Electrical and Electronics Engineers Inc. 2023. (2023 5th International Conference on Problems of Cybernetics and Informatics, PCI 2023). doi: 10.1109/PCI60110.2023.10325920

Development of Satellite Attitude Controller with TRIAD and Particle Swarm Optimization Using Only Magnetic Actuators

Abstract

Publication series

Conference

Bibliographical note

Keywords

Access to Document

Other files and links

Fingerprint

Cite this