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On the Stability of Steady Motions of Solar-Sail Satellite

In: Computer Algebra in Scientific Computing CASC 2001

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  • Larissa Bourlakova

    (Institute of Systems Dynamics and Control Theory SB RAS)

Abstract

A satellite with solar sail moving along a circular heliocentric orbit is considered. A complete set of steady motions for such a system has been obtained, and Lyapunov’s method has been employed to investigate their stability. The sufficient conditions are compared with the necessary ones. To the end of solving the problem, the capabilities of the software “Stability” for symbolic computations have been used [1].

Suggested Citation

  • Larissa Bourlakova, 2001. "On the Stability of Steady Motions of Solar-Sail Satellite," Springer Books, in: Victor G. Ganzha & Ernst W. Mayr & Evgenii V. Vorozhtsov (ed.), Computer Algebra in Scientific Computing CASC 2001, pages 75-82, Springer.
    • Handle: RePEc:spr:sprchp:978-3-642-56666-0_6
    DOI: 10.1007/978-3-642-56666-0_6
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