Stability analysis of coupled orbit-attitude dynamics around asteroids using finite-time Lyapunov exponents

Shota Kikuchi, Yuichi Tsuda, Jun'ichiro Kawaguchi

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Abstract

This study investigates coupled orbit-attitude dynamics around asteroids subject to solar radiation pressure and gravity irregularities. The solutions of Sun-synchronous orbits with Sun-tracking attitude motion are analytically derived by applying linearization and averaging. To verify the validity of the analytical solutions, numerical simulations are performed based on non-linear coupled orbit-attitude equations of motion. In addition, the stability of such coupled motion is analyzed using finite-time Lyapunov exponents. It is demonstrated that the Sun-synchronous orbit-attitude coupled motions exhibit long-term stability under certain conditions, and thus, these motions are useful and feasible options for asteroid missions.

Original languageEnglish
Title of host publicationASTRODYNAMICS 2017
EditorsJohn H. Seago, Nathan J. Strange, Daniel J. Scheeres, Jeffrey S. Parker
PublisherUnivelt Inc.
Pages2081-2100
Number of pages20
ISBN (Print)9780877036456
Publication statusPublished - 2018
Externally publishedYes
EventAAS/AIAA Astrodynamics Specialist Conference, 2017 - Stevenson, United States
Duration: 2017 Aug 202017 Aug 24

Publication series

NameAdvances in the Astronautical Sciences
Volume162
ISSN (Print)0065-3438

Conference

ConferenceAAS/AIAA Astrodynamics Specialist Conference, 2017
CountryUnited States
CityStevenson
Period17/8/2017/8/24

ASJC Scopus subject areas

  • Aerospace Engineering
  • Space and Planetary Science

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