Abstract
The dynamics of a satellite with a gravitational stabilization system is investigated. The parameters providing minimum duration of the natural oscillation damping of the system are determined. Main attention is given to the analysis of oscillation of the system in the orbit plane.
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References
Okhotsimsky, D. E. and Sarychev, V. A., ‘A Gravitational Stabilization System of the Artificial Satellites’, in Col. Artificial Earth Satellite, Vol. 16, U.S.S.R. Academy of Sciences, Moscow, 1963, p. 5–9.
Sarychev, V. A., ‘Investigation of the Dynamics of a Gravitational Stabilization System’, in Col. Artificial Earth Satellite, Vol. 16, U.S.S.R. Academy of Sciences, Moscow, 1963, p. 10–33.
Tsypkin, Ja. Z. and Bromberg, P. V., ‘The Degree of Stability of Linear System’, NISO, N9, 1946.
Zajac, E. E., ‘Damping of a Gravitationally Oriented Two-Body Satellite’, ARS J 32 (1962) 1871–1875.
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© 1970 D. Reidel Publishing Company, Dordrecht, Holland
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Sarychev, V.A. (1970). Satellite Gravitational Stabilization Systems with Maximum Damping Rate. In: Partel, G.A. (eds) Space Engineering. Astrophysics and Space Science Library, vol 15. Springer, Dordrecht. https://doi.org/10.1007/978-94-011-7551-7_40
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DOI: https://doi.org/10.1007/978-94-011-7551-7_40
Publisher Name: Springer, Dordrecht
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