Satellite Formation Flight via Thrusters and Proportional-Integral-Derivative Control Approaches

Tuncay Yunus Erkec; Chingiz Hajiyev

doi:10.1007/978-3-031-29933-9_5

Satellite Formation Flight via Thrusters and Proportional-Integral-Derivative Control Approaches

Tuncay Yunus Erkec^*, Chingiz Hajiyev

^*Corresponding author for this work

Department of Aeronautical Engineering

Turkish National Defence University

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

Abstract

This chapter is focused to control of relative satellite vector estimations with various Kalman filter (KF) and Proportional-Integral-Derivative (PID) approaches. The identical 3U target and follower satellites orbits and initial conditions are simulated according with desired formation geometry limitations. In this study, target and follower satellites states are determined as derived simulation data. The various satellites thruster’s scenario is analyzed with various relative state estimation which use Kalman filters. The novel methods, which satellites and relative orbit estimation are determined via two stages, are inputted to the control section of follower satellites within formation flight of satellites architecture.

Original language	English
Title of host publication	Sustainable Aviation
Publisher	Springer Nature
Pages	37-44
Number of pages	8
DOIs	https://doi.org/10.1007/978-3-031-29933-9_5
Publication status	Published - 2023

Publication series

Name	Sustainable Aviation
Volume	Part F4673
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

Cluster satellites
Formation flight
GPS
PID control
Pseudo-ranging model
Relative vavigation
Satellite

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10.1007/978-3-031-29933-9_5

Cite this

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abstract = "This chapter is focused to control of relative satellite vector estimations with various Kalman filter (KF) and Proportional-Integral-Derivative (PID) approaches. The identical 3U target and follower satellites orbits and initial conditions are simulated according with desired formation geometry limitations. In this study, target and follower satellites states are determined as derived simulation data. The various satellites thruster{\textquoteright}s scenario is analyzed with various relative state estimation which use Kalman filters. The novel methods, which satellites and relative orbit estimation are determined via two stages, are inputted to the control section of follower satellites within formation flight of satellites architecture.",

keywords = "Cluster satellites, Formation flight, GPS, PID control, Pseudo-ranging model, Relative vavigation, Satellite",

author = "Erkec, \{Tuncay Yunus\} and Chingiz Hajiyev",

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AU - Hajiyev, Chingiz

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PY - 2023

Y1 - 2023

N2 - This chapter is focused to control of relative satellite vector estimations with various Kalman filter (KF) and Proportional-Integral-Derivative (PID) approaches. The identical 3U target and follower satellites orbits and initial conditions are simulated according with desired formation geometry limitations. In this study, target and follower satellites states are determined as derived simulation data. The various satellites thruster’s scenario is analyzed with various relative state estimation which use Kalman filters. The novel methods, which satellites and relative orbit estimation are determined via two stages, are inputted to the control section of follower satellites within formation flight of satellites architecture.

AB - This chapter is focused to control of relative satellite vector estimations with various Kalman filter (KF) and Proportional-Integral-Derivative (PID) approaches. The identical 3U target and follower satellites orbits and initial conditions are simulated according with desired formation geometry limitations. In this study, target and follower satellites states are determined as derived simulation data. The various satellites thruster’s scenario is analyzed with various relative state estimation which use Kalman filters. The novel methods, which satellites and relative orbit estimation are determined via two stages, are inputted to the control section of follower satellites within formation flight of satellites architecture.

KW - Cluster satellites

KW - Formation flight

KW - GPS

KW - PID control

KW - Pseudo-ranging model

KW - Relative vavigation

KW - Satellite

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M3 - Chapter

AN - SCOPUS:105006794672

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SP - 37

EP - 44

BT - Sustainable Aviation

PB - Springer Nature

ER -

Satellite Formation Flight via Thrusters and Proportional-Integral-Derivative Control Approaches

Abstract

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Keywords

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