Stabilization of a symmetric artificial sun satellite in a light pressure force field

Details Stabilization of a symmetric artificial sun satellite in a light pressure force field Stabilization of a symmetric artificial sun satellite in a light pressure force field

Oct 1992

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1992mvsmm...5...53a&link_type=abstract

Moskovskii Universitet, Vestnik, Seriia 1 - Matematika, Mekhanika (ISSN 0579-9368), no. 5, p. 53-59.

Other

Orbital Mechanics, Radiation Pressure, Satellite Perturbation, Solar Orbits, Spacecraft Stability, Circular Orbits, Gravitational Effects, Satellite Orbits

Scientific paper

The paper is concerned with the problem of the motion of a dynamically symmetric satellite along a circular heliocentric orbit in gravitational and light pressure force fields. Three stationary positions of the satellite symmetry axis in orbital coordinates are determined, and it is proved that no other stationary positions exist. For the stationary positions, regions where the sufficient stability conditions are satisfied are determined.

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