Influence of constant torque on equilibria of satellite in circular orbit

DOI10.1023/B:CELE.0000005713.66553.88zbMath1106.70331OpenAlexW2076535383MaRDI QIDQ1764123

Pedro Paglione, Vasily A. Sarychev, Anna D. Guerman

Publication date: 23 February 2005

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

Full work available at URL: https://doi.org/10.1023/b:cele.0000005713.66553.88

zbMATH Keywords

two-body problemperiodic trajectories

Mathematics Subject Classification ID

Two-body problems (70F05) Orbital mechanics (70M20) Stability problems in rigid body dynamics (70E50)

Related Items (3)

Investigation of the influence of constant torque on equilibrium orientations of a satellite moving in a circular orbit with the use of computer algebra methods ⋮ Satellite dynamics due to gravity and constant torques ⋮ Analysis of analytical attitude propagators for spin-stabilized satellites

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