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Equilibrium attitude and nonlinear attitude stability of a spacecraft on a stationary orbit around an asteroid
Institution:Department of Guidance, Navigation and Control, School of Astronautics, Beijing University of Aeronautics and Astronautics, Room B1024, New Main Building, 100191 Beijing, China
Abstract:
Keywords:Asteroids  Equilibrium attitude  Nonlinear stability  Geometric mechanics  Non-canonical Hamiltonian structure  Energy-Casimir method
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