Effects of gravity-gradient torque on the rotational motion of A triaxial satellite in a precessing elliptic orbit

DOI10.1007/BF01227777zbMath0247.70024OpenAlexW4250711845MaRDI QIDQ5660561

Publication date: 1972

Published in: Celestial Mechanics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/bf01227777

Mathematics Subject Classification ID

Asymptotic approximations, asymptotic expansions (steepest descent, etc.) (41A60) Hamilton-Jacobi equations in mechanics (70H20) Orbital mechanics (70M20) Dynamics of a rigid body and of multibody systems (70E99) Canonical and symplectic transformations for problems in Hamiltonian and Lagrangian mechanics (70H15)

Related Items (11)

The translational-rotational motion of an Earth spheroid satellite ⋮ The triaxiality role in the spin-orbit dynamics of a rigid body ⋮ Long-term attitude dynamics of space debris in Sun-synchronous orbits: Cassini cycles and chaotic stabilization ⋮ Regimes of regular and chaotic motion of gyrostats in the central gravity field ⋮ Higher-order analytical attitude propagation of an oblate rigid body under gravity-gradient torque ⋮ A complex analytic solution for the attitude motion of a near-symmetric rigid body under body-fixed torques ⋮ Perturbation formulations for satellite attitude dynamics ⋮ Poisson equations of rotational motion for a rigid triaxial body with application to a tumbling artificial satellite ⋮ Attitude dynamics of a rigid body on a Keplerian orbit: A simplification ⋮ The eccentric case of a fast-rotating, gravity-gradient-perturbed satellite attitude solution ⋮ Study of the terms of coupling between rotational and translational motions

Cites Work

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