Feedback stabilization of displaced periodic orbits: applications to binary asteroids

Jules Simo; Colin McInnes

doi:10.1016/j.actaastro.2013.11.026

Feedback stabilization of displaced periodic orbits: applications to binary asteroids

Jules Simo, Colin McInnes

Mechanical And Aerospace Engineering

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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.

Original language	English
Pages (from-to)	106-115
Number of pages	10
Journal	Acta Astronautica
Volume	96
Early online date	27 Nov 2013
DOIs	https://doi.org/10.1016/j.actaastro.2013.11.026
Publication status	Published - Mar 2014
Event	22nd AAS/AIAA Spaceflight Mechanics Meeting - Charleston, South Carolina, United States Duration: 29 Jan 2012 → 2 Feb 2012

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

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10.1016/j.actaastro.2013.11.026

Simo-J-&-McInnes-CR-Acta-Astro-Feedback-stabilization-displaced-periodic-orbits-application-binary-asteroid-Mar-2014Accepted author manuscript, 325 KBLicence: CC BY-NC-ND 4.0

Cite this

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title = "Feedback stabilization of displaced periodic orbits: applications to binary asteroids",

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. ",

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",

author = "Jules Simo and Colin McInnes",

year = "2014",

month = mar,

doi = "10.1016/j.actaastro.2013.11.026",

language = "English",

volume = "96",

pages = "106--115",

journal = "Acta Astronautica",

issn = "0094-5765",

note = "22nd AAS/AIAA Spaceflight Mechanics Meeting ; Conference date: 29-01-2012 Through 02-02-2012",

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TY - JOUR

T1 - Feedback stabilization of displaced periodic orbits

T2 - 22nd AAS/AIAA Spaceflight Mechanics Meeting

AU - Simo, Jules

AU - McInnes, Colin

PY - 2014/3

Y1 - 2014/3

N2 - 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.

AB - 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.

KW - feedback control

KW - linearisation techniques

KW - stabilisation

KW - binary asteroid systems

KW - non-Keplerian orbits

KW - circular restricted three-body problem

KW - circular restricted Earth-Moon system (CRTBP)

KW - asymptotic stability

UR - http://www.sciencedirect.com/science/article/pii/S0094576513004293

U2 - 10.1016/j.actaastro.2013.11.026

DO - 10.1016/j.actaastro.2013.11.026

M3 - Article

SN - 0094-5765

VL - 96

SP - 106

EP - 115

JO - Acta Astronautica

JF - Acta Astronautica

Y2 - 29 January 2012 through 2 February 2012

ER -

Feedback stabilization of displaced periodic orbits: applications to binary asteroids

Abstract

Keywords

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