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

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Official URL: https://doi.org/10.1016/j.actaastro.2013.11.026

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.

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Simo, Jules

and McInnes, Colin;

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Item metadata

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:	05 Apr 2021 00:24
Related URLs:	Journal or Publication
URI:	https://strathprints.strath.ac.uk/id/eprint/48074

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