Hamiltonian and chaotic attitude dynamics of an orbiting gyrostat satellite under gravity-gradient torques
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Publication:1413518
DOI10.1016/S0167-2789(03)00241-0zbMath1051.70018OpenAlexW2062181694MaRDI QIDQ1413518
Soonhie Tan, Andrew Y. T. Leung, J. L. Kuang
Publication date: 16 November 2003
Published in: Physica D (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1016/s0167-2789(03)00241-0
Hamilton's equations (70H05) Orbital mechanics (70M20) Dynamical systems in classical and celestial mechanics (37N05)
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Chaos and optimal control of steady-state rotation of a satellite-gyrostat on a circular orbit, Attitude evolution of a dual-liquid-filled spacecraft with internal energy dissipation, Function projective synchronization of fractional order satellite system and its stability analysis for incommensurate case, Chaos analysis in attitude dynamics of a flexible satellite, Chaotic satellite attitude control by adaptive approach
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