Controllability analysis of propellant-free satellite formation flight

Mohamed Shouman, Mai Bando, Shinji Hokamoto

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

1 被引用数 (Scopus)

抄録

This paper proposes the controllability analysis of relative motion using different configurations for hybrid control actions of space environmental forces. It tends to present a minimal configuration for the missions exploiting these forces. It illustrates the constraints in each space environmental force and analyzes the integration between these forces to achieve full controllability of the satellite formation flight for near-circular low earth orbits with different orbit configurations. The paper implements a Kalman decomposition approach to decompose the system into controllable and uncontrollable subspaces for linear time-invariant control actions. Numerical simulations are investigated to study the controllability analysis for nonlinear models and substantiate the success of the controllability study for all hybrid control actions with different orbit configurations.

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3577-3596
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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