Floquet modes and stability analysis of periodic orbit-attitude solutions along Earth–Moon halo orbits

نویسندگان

چکیده

Abstract Future space programmes pose some interesting research problems in the field of non-Keplerian dynamics, being Moon and cislunar central proposed roadmap for future exploration. In these regards, deployment a station on orbit lunar vicinity is fundamental milestone to be achieved. The paper investigates natural orbit-attitude dynamics attitude stabilisation coupled motions extended bodies Earth–Moon system. discussion carried out analysing phase constituted by both orbital rotational periodic spacecraft orbits. Floquet theory applied solutions proximity, characterise their stability properties manifolds, which are discussed analysed focusing dynamical features applicable environment. Attitude methods developed, with particular attention spin-stabilised solutions. Periodic studied highlight possible favourable conditions that may exploited host simplified control action. focus analysis dedicated halo orbits near-rectilinear circular restricted three-body problem

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ژورنال

عنوان ژورنال: Celestial Mechanics and Dynamical Astronomy

سال: 2021

ISSN: ['1572-9478', '0923-2958']

DOI: https://doi.org/10.1007/s10569-021-10030-y