Model predictive approach for detumbling an underactuated satellite

研究成果: Chapter in Book/Report/Conference proceedingConference contribution

抄録

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.

本文言語英語
ホスト出版物のタイトルAIAA Scitech 2020 Forum
出版社American Institute of Aeronautics and Astronautics Inc, AIAA
ISBN(印刷版)9781624105951
DOI
出版ステータス出版済み - 2020
イベントAIAA Scitech Forum, 2020 - Orlando, 米国
継続期間: 1 6 20201 10 2020

出版物シリーズ

名前AIAA Scitech 2020 Forum
1 PartF

会議

会議AIAA Scitech Forum, 2020
Country米国
CityOrlando
Period1/6/201/10/20

All Science Journal Classification (ASJC) codes

  • Aerospace Engineering

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