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Time-delayed feedback control in astrodynamics

Biggs, James and McInnes, Colin (2009) Time-delayed feedback control in astrodynamics. Journal of Guidance, Control and Dynamics, 32 (6). pp. 1804-1811. ISSN 0731-5090

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    Abstract

    In this paper we present time-delayed feedback control (TDFC) for the purpose of autonomously driving trajectories of nonlinear systems into periodic orbits. As the generation of periodic orbits is a major component of many problems in astodynamics we propose this method as a useful tool in such applications. To motivate the use of this method we apply it to a number of well known problems in the astrodynamics literature. Firstly, TDFC is applied to control in the chaotic attitude motion of an asymmetric satellite in an elliptical orbit. Secondly, we apply TDFC to the problem of maintaining a spacecraft in a periodic orbit about a body with large ellipticity (such as an asteroid) and finally, we apply TDFC to eliminate the drift between two satellites in low Earth orbits to ensure their relative motion is bounded.

    Item type: Article
    ID code: 12921
    Keywords: non-linear systems, periodic orbits, astrodynamics, Mechanical engineering and machinery, Motor vehicles. Aeronautics. Astronautics, 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
    Related URLs:
      Depositing user: Ms Katrina May
      Date Deposited: 19 Aug 2009 16:27
      Last modified: 28 Mar 2014 22:07
      URI: http://strathprints.strath.ac.uk/id/eprint/12921

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