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On stability of limit cycles in stabilization systems of spacecrafts with elastic rods

  • Control Systems of Moving Objects
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Abstract

Systems of differential motion equations perturbed by moment of external forces for spacecrafts with elastic rods and perfectly rigid bodies at their ends are constructed. Limit cycles and transition processes in the nonlinear control system with account of delay time in gas jet engines are simulated. A method of rigorous investigation of stability of limit cycles based on previously proved theorem on stable quasi-polynomial is proposed.

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Authors and Affiliations

  1. Saratov State Technical University, Saratov, 410016, Russia

    D. K. Andreichenko & K. P. Andreichenko

Authors
  1. D. K. Andreichenko
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  2. K. P. Andreichenko
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Original Russian Text © D.K. Andreichenko, K.P. Andreichenko, 2007, published in Izvestiya Akademii Nauk. Teoriya i Sistemy Upravleniya, 2007, No. 5, pp. 137–149.

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Andreichenko, D.K., Andreichenko, K.P. On stability of limit cycles in stabilization systems of spacecrafts with elastic rods. J. Comput. Syst. Sci. Int. 46, 802–814 (2007). https://doi.org/10.1134/S1064230707050127

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  • DOI: https://doi.org/10.1134/S1064230707050127

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