Relative equilibria of a satellite subjected to gravitational and aerodynamic torques
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Publication:1582383
DOI10.1023/A:1008389730047zbMath0959.70018OpenAlexW1630312668MaRDI QIDQ1582383
S. A. Mirer, Vasily A. Sarychev
Publication date: 2 May 2001
Published in: Celestial Mechanics and Dynamical Astronomy (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1023/a:1008389730047
satelliteLyapunov methodattitude motioncircular orbitgravitational torqueaerodynamic torqueexistence of one-parameter families of stationary solutionsnumber of isolated equilibriasufficient conditions for stability of isolated equilibria
Related Items (4)
Investigation of equilibria of a satellite subjected to gravitational and aerodynamic torques ⋮ Equilibria of a satellite subjected to gravitational and aerodynamic torques with pressure center in a principal plane of inertia ⋮ A Symbolic Investigation of the Influence of Aerodynamic Forces on Satellite Equilibria ⋮ Gravitational stabilization of a satellite using a movable mass
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