Elimination of the nodes when the satellite is a non spherical rigid body
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Publication:1824439
DOI10.1007/BF00051485zbMath0682.70026MaRDI QIDQ1824439
Maria-Eugenia Sansaturio, José Manuel Ferrándiz
Publication date: 1989
Published in: Celestial Mechanics and Dynamical Astronomy (Search for Journal in Brave)
Orbital mechanics (70M20) Canonical and symplectic transformations for problems in Hamiltonian and Lagrangian mechanics (70H15)
Related Items (6)
\((SO(3) \times \mathbb{T}^4)\)-reduction and relative equilibria for a radial axisymmetric intermediary model for roto-orbital motion ⋮ The triaxiality role in the spin-orbit dynamics of a rigid body ⋮ Complex variables approach to the short-axis-mode rotation of a rigid body ⋮ Short-axis-mode rotation of a free rigid body by perturbation series ⋮ Study of the roto-orbital motion using intermediaries: numerical experiments ⋮ On the roto-translatory motion of a satellite of an oblate primary
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