Feedback stabilization of displaced periodic orbits : applications to binary asteroids

Simo, Jules and McInnes, Colin (2014) Feedback stabilization of displaced periodic orbits : applications to binary asteroids. Acta Astronautica, 96. pp. 106-115. ISSN 0094-5765 (https://doi.org/10.1016/j.actaastro.2013.11.026)

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Abstract

This paper investigates displaced periodic orbits at linear order in the circular restricted Earth-Moon system (CRTBP), where the third massless body utilises a hybrid of solar sail and solar electric propulsion (SEP). A feedback linearisation control scheme is implemented to perform stabilisation and trajectory tracking for the nonlinear system. Next, attention is directed to binary asteroid systems as an application of the restricted problem. The idea of combining a solar sail with an SEP auxiliary system to obtain a hybrid sail system is important especially due to the challenges of performing complex trajectories.

ORCID iDs

Simo, Jules ORCID logoORCID: https://orcid.org/0000-0002-1489-5920 and McInnes, Colin;
  • Item type:Article
    ID code:48074
    Dates:
    Date
    Event
    March 2014
    Published
    27 November 2013
    Published Online
    19 November 2013
    Accepted
    Keywords:feedback control, linearisation techniques, stabilisation, binary asteroid systems , non-Keplerian orbits, circular restricted three-body problem, circular restricted Earth-Moon system (CRTBP) , asymptotic stability, Mechanical engineering and machinery, Motor vehicles. Aeronautics. Astronautics, Mechanical Engineering, Aerospace Engineering, Control and Systems Engineering
    Subjects:Technology > Mechanical engineering and machinery
    Technology > Motor vehicles. Aeronautics. Astronautics
    Department:Faculty of Engineering > Mechanical and Aerospace Engineering
    Depositing user: Pure Administrator
    Date deposited:14 May 2014 09:41
    Last modified:16 Nov 2021 01:43
    Related URLs:
    URI:https://strathprints.strath.ac.uk/id/eprint/48074
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