Motion of a satellite with a permanent magnet relative to the center of mass

Details Motion of a satellite with a permanent magnet relative to the center of mass Motion of a satellite with a permanent magnet relative to the center of mass

Jul 1986

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1986kosis..24..527s&link_type=abstract

Kosmicheskie Issledovaniia (ISSN 0023-4206), vol. 24, July-Aug. 1986, p. 527-543. In Russian.

Physics

Center Of Mass, Magnetic Control, Satellite Attitude Control, Spacecraft Motion, Aerodynamic Forces, Eccentric Orbits, Equations Of Motion, Gravitational Effects, Magnetic Moments, Satellite Orbits

Scientific paper

A satellite with a magnetic attitude control system experiences undamped forces oscillations in orbital motion due to nonuniform variations of the direction and strength vector of the geomagnetic field at the current point of the orbit. In the framework of a stationary model of the geomagnetic field, the analysis of the forced motions of a satellite with a permanent magnet is reduced to the investigation of its periodic motions; allowance is made for the effects of gravitational and aerodynamic moments as well as for the effect of orbit eccentricity.

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