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Journal of Automation and Information Sciences
SJR: 0.238 SNIP: 0.464 CiteScore™: 0.27

ISSN Imprimir: 1064-2315
ISSN On-line: 2163-9337

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Journal of Automation and Information Sciences

DOI: 10.1615/JAutomatInfScien.v49.i9.30
pages 29-41

Synthesis of Algorithms for Spacecraft Attitude Control Based on Generalizations of the Direct Lyapunov Method

Victor V. Volosov
Institute of Space Research of National Academy of Sciences of Ukraine and National Space Agency of Ukraine, Kyiv
Vladimir N. Shevchenko
Institute of Space Research of National Academy of Sciences of Ukraine and National Space Agency of Ukraine, Kyiv, Ukraine

RESUMO

The well-known generalizations of the direct Lyapunov method for investigation of the stability of invariant sets of dynamic systems are applied to the problem of synthesis of spacecraft (SC) attitude control. Generalizations of the existing algorithms of SC attitude control and stabilization with respect to an inertial coordinate system (CS) are obtained. New algorithms of SC attitude control and stabilization with respect to a rotating (orbital) CS are proposed. The corresponding algorithms for an inertial CS are particular cases of these algorithms. The efficiency of the algorithms is illustrated by computer modeling of the dynamics of SC attitude control systems.


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