Analytical and semi-analytical analysis of an artificial satellite's rotational motion

DOI10.1023/A:1008358801859zbMath0971.70024OpenAlexW1537592064MaRDI QIDQ1576479

Rodolpho Vilhena de Moraes, Maria Cecília F. P. S. Zanardi

Publication date: 14 August 2000

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

Full work available at URL: https://doi.org/10.1023/a:1008358801859

zbMATH Keywords

rotational motionsolar radiation pressureAndoyer variablesgravity gradientcylindical artificial satelliteEarth's shadowLagrange's method of variations of parameterssemi-analytical proceduresolar radiation torque

Mathematics Subject Classification ID

Celestial mechanics (70F15) Orbital mechanics (70M20) Waves and radiation in optics and electromagnetic theory (78A40)

Related Items (5)

The theory of canonical perturbations applied to attitude dynamics and to the Earth rotation. Osculating and nonosculating Andoyer variables ⋮ The translational-rotational motion of an Earth spheroid satellite ⋮ Higher-order analytical attitude propagation of an oblate rigid body under gravity-gradient torque ⋮ The eccentric case of a fast-rotating, gravity-gradient-perturbed satellite attitude solution ⋮ Analysis of analytical attitude propagators for spin-stabilized satellites

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