Investigation of equilibria of a satellite subjected to gravitational and aerodynamic torques

DOI10.1007/S10569-006-9064-3zbMath1117.70026OpenAlexW1975712131MaRDI QIDQ871314

E. K. Duarte, S. A. Mirer, A. A. Degtyarev, Vasily A. Sarychev

Publication date: 16 March 2007

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

Full work available at URL: https://doi.org/10.1007/s10569-006-9064-3

zbMATH Keywords

SatelliteAerodynamic torqueAttitude motionConditions of stabilityEquilibrium orientationGravitational torque

Mathematics Subject Classification ID

Stability for nonlinear problems in mechanics (70K20) Orbital mechanics (70M20)

Related Items (4)

Equilibria of a satellite subjected to gravitational and aerodynamic torques with pressure center in a principal plane of inertia ⋮ A Symbolic Investigation of the Influence of Aerodynamic Forces on Satellite Equilibria ⋮ Qualitative Analysis of the Reyman – Semenov–Tian–Shansky Integrable Case of the Generalized Kowalewski Top ⋮ Attitude stability of artificial satellites subject to gravity gradient torque

Cites Work

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• Relative equilibria of a satellite subjected to gravitational and aerodynamic torques
• Aerodynamic Influences on Satellite Librations
• Gravity gradient stabilization of the salyut-soyuz orbital complex
• The passive attitude motion of the orbital stations Salyut-6 and Salyut-7
• Gravity gradient stabilization of large space stations
• Stabilization due to gyroscopic coupling in dual-spin satellites subject to gravitational torques
• On the effect of aerodynamic and gravitational torques on the attitude stability of satellites.

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