Model predictive approach for detumbling an underactuated satellite

Kota Kondo; Yasuhiro Yoshimura; Mai Bando; Shuji Nagasaki; Toshiya Hanada

doi:10.2514/6.2020-1433

Model predictive approach for detumbling an underactuated satellite

Kota Kondo, Yasuhiro Yoshimura, Mai Bando, Shuji Nagasaki, Toshiya Hanada

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

1 Citation (Scopus)

Abstract

This research proposes an innovative approach to detumble satellites’ triple-axis angular velocities with only one single-axis magnetic torquer. Since magnetic torque is generated perpendicularly to magnetorquers, no intended control torque along the magnetorquer can be produced, which makes systems underactuated. Our paper introduces a control method using Model Predictive Control (MPC) and compares it with B-dot control algorithm. By applying these control laws to Kyushu University Light Curve Inversion (Q-Li) Demonstration Satellite in numerical simulations, we describe the applicability of these control laws to underactuated systems.

Original language	English
Title of host publication	AIAA Scitech 2020 Forum
Publisher	American Institute of Aeronautics and Astronautics Inc, AIAA
ISBN (Print)	9781624105951
DOIs	https://doi.org/10.2514/6.2020-1433
Publication status	Published - 2020
Event	AIAA Scitech Forum, 2020 - Orlando, United States Duration: Jan 6 2020 → Jan 10 2020

Publication series

Name	AIAA Scitech 2020 Forum
Volume	1 PartF

Conference

Conference	AIAA Scitech Forum, 2020
Country/Territory	United States
City	Orlando
Period	1/6/20 → 1/10/20

All Science Journal Classification (ASJC) codes

Aerospace Engineering

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10.2514/6.2020-1433

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@inproceedings{2d75856f86fd477ab817199662d3ab57,

title = "Model predictive approach for detumbling an underactuated satellite",

abstract = "This research proposes an innovative approach to detumble satellites{\textquoteright} triple-axis angular velocities with only one single-axis magnetic torquer. Since magnetic torque is generated perpendicularly to magnetorquers, no intended control torque along the magnetorquer can be produced, which makes systems underactuated. Our paper introduces a control method using Model Predictive Control (MPC) and compares it with B-dot control algorithm. By applying these control laws to Kyushu University Light Curve Inversion (Q-Li) Demonstration Satellite in numerical simulations, we describe the applicability of these control laws to underactuated systems.",

author = "Kota Kondo and Yasuhiro Yoshimura and Mai Bando and Shuji Nagasaki and Toshiya Hanada",

note = "Publisher Copyright: {\textcopyright} 2020, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.; AIAA Scitech Forum, 2020 ; Conference date: 06-01-2020 Through 10-01-2020",

year = "2020",

doi = "10.2514/6.2020-1433",

language = "English",

isbn = "9781624105951",

series = "AIAA Scitech 2020 Forum",

publisher = "American Institute of Aeronautics and Astronautics Inc, AIAA",

booktitle = "AIAA Scitech 2020 Forum",

}

TY - GEN

T1 - Model predictive approach for detumbling an underactuated satellite

AU - Kondo, Kota

AU - Yoshimura, Yasuhiro

AU - Bando, Mai

AU - Nagasaki, Shuji

AU - Hanada, Toshiya

PY - 2020

Y1 - 2020

N2 - This research proposes an innovative approach to detumble satellites’ triple-axis angular velocities with only one single-axis magnetic torquer. Since magnetic torque is generated perpendicularly to magnetorquers, no intended control torque along the magnetorquer can be produced, which makes systems underactuated. Our paper introduces a control method using Model Predictive Control (MPC) and compares it with B-dot control algorithm. By applying these control laws to Kyushu University Light Curve Inversion (Q-Li) Demonstration Satellite in numerical simulations, we describe the applicability of these control laws to underactuated systems.

AB - This research proposes an innovative approach to detumble satellites’ triple-axis angular velocities with only one single-axis magnetic torquer. Since magnetic torque is generated perpendicularly to magnetorquers, no intended control torque along the magnetorquer can be produced, which makes systems underactuated. Our paper introduces a control method using Model Predictive Control (MPC) and compares it with B-dot control algorithm. By applying these control laws to Kyushu University Light Curve Inversion (Q-Li) Demonstration Satellite in numerical simulations, we describe the applicability of these control laws to underactuated systems.

UR - http://www.scopus.com/inward/record.url?scp=85091939889&partnerID=8YFLogxK

UR - http://www.scopus.com/inward/citedby.url?scp=85091939889&partnerID=8YFLogxK

U2 - 10.2514/6.2020-1433

DO - 10.2514/6.2020-1433

M3 - Conference contribution

AN - SCOPUS:85091939889

SN - 9781624105951

T3 - AIAA Scitech 2020 Forum

BT - AIAA Scitech 2020 Forum

PB - American Institute of Aeronautics and Astronautics Inc, AIAA

T2 - AIAA Scitech Forum, 2020

Y2 - 6 January 2020 through 10 January 2020

ER -

Model predictive approach for detumbling an underactuated satellite

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