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Two spherical satellite relative motion control in formation flying via variable surface reflectivity
R. V. Dosaev, S. S. Tkachev
Abstract:
The possibility of two spherical satellites relative motion control using solar radiation pressure is considered. The source of control is a variable reflectivity of one of the satellites surface. The perturbations of $\mathrm{J}_2$ harmonic and small eccentricity of satellites are taken into account.
Keywords:
spherical solar sail, satellite relative motion control, variable surface reflectivity.
Citation:
R. V. Dosaev, S. S. Tkachev, “Two spherical satellite relative motion control in formation flying via variable surface reflectivity”, Keldysh Institute preprints, 2016, 107, 28 pp.
Linking options:
https://www.mathnet.ru/eng/ipmp2181 https://www.mathnet.ru/eng/ipmp/y2016/p107
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Statistics & downloads: |
Abstract page: | 68 | Full-text PDF : | 26 | References: | 12 |
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