Output regulation control for satellite formation flying using differential drag

Mohamed Shouman, Mai Bando, Shinji Hokamoto

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

抄録

This paper proposes a new hybrid control action of differentials aerodynamic drag and thrusters to control satellite formation flying in low Earth orbits. Parameterized output regulation algorithm for formation flying missions is developed based on the Schweighart-Sedwick relative dynamics equations. It is implemented to precisely track the different trajectories of reference relative motion and eliminates the effects of the J2 perturbations. Parametric Lyapunov algebraic equation is derived to ensure the stability of the linear relative model subject to saturated inputs. The main goal of this study is to approve the viability of using the differentials in aerodynamic drag to precisely control different formation flying missions. Numerical simulations using a high fidelity relative dynamics model are implemented to analyze the performance of the proposed control algorithm in comparison with the linear quadratic regulator algorithm for actual satellite parameters. The paper exploits a high-precision orbit propagator model to verify the robustness of the control algorithm.

本文言語英語
ホスト出版物のタイトルSpaceflight Mechanics 2019
編集者Francesco Topputo, Andrew J. Sinclair, Matthew P. Wilkins, Renato Zanetti
出版社Univelt Inc.
ページ3433-3452
ページ数20
ISBN(印刷版)9780877036593
出版ステータス出版済み - 2019
イベント29th AAS/AIAA Space Flight Mechanics Meeting, 2019 - Maui, 米国
継続期間: 1 13 20191 17 2019

出版物シリーズ

名前Advances in the Astronautical Sciences
168
ISSN(印刷版)0065-3438

会議

会議29th AAS/AIAA Space Flight Mechanics Meeting, 2019
国/地域米国
CityMaui
Period1/13/191/17/19

All Science Journal Classification (ASJC) codes

  • 航空宇宙工学
  • 宇宙惑星科学

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