Equilibria of a satellite subject to gravitational and constant torques.

Details Equilibria of a satellite subject to gravitational and constant torques. Equilibria of a satellite subject to gravitational and constant torques.

Oct 1994

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1994kosis..32...43s&link_type=abstract

Kosmicheskie Issledovaniia, Tom 32, Vyp. 4 - 5, p. 43 - 50

Physics

Artificial Satellites: Equilibria, Artificial Satellites: Orbit Theory

Scientific paper

The equilibria of a satellite subject to gravitational and constant torques in a circular orbit are investigated. A method to investigate all the equilibrium positions of a satellite with a prescribed constant torque and prescribed central moments of inertia is presented. It is shown that a satellite with a small constant torque has 24 equilibrium positions. The number of equilibrium positions is reduced to zero as the constant torque increases. Numerical investigations of the equilibrium positions are performed.

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