Attitude dynamics of a rigid body on a Keplerian orbit: A simplification

DOI10.1007/BF00692512zbMath0767.70005OpenAlexW2008691587MaRDI QIDQ1209268

Antonio Elipe, Mercedes Arribas

Publication date: 16 May 1993

Published in: Celestial Mechanics and Dynamical Astronomy (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/bf00692512

zbMATH Keywords

moments of inertiatriaxial rigid bodyLie seriesEuler-Poinsot model

Mathematics Subject Classification ID

Free motion of a rigid body (70E15) Hamilton's equations (70H05) Two-body problems (70F05) Orbital mechanics (70M20)

Related Items (3)

Motions about a fixed point by hypergeometric functions: new non-complex analytical solutions and integration of the herpolhode ⋮ The eccentric case of a fast-rotating, gravity-gradient-perturbed satellite attitude solution ⋮ Chaos analysis in attitude dynamics of a flexible satellite

Cites Work

• Simplify or perish
• The General Problem of the Motion of Coupled Rigid Bodies about a Fixed Point
• Effects of gravity-gradient torque on the rotational motion of A triaxial satellite in a precessing elliptic orbit

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