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IssuesArchive of Issues2002-2pp.13-18

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I. A. Mukhametzyanov, "On the stabilization of the cylindrical precession of a satellite in an elliptic orbit," Mech. Solids. 37 (2), 13-18 (2002)
Year 2002 Volume 37 Number 2 Pages 13-18
Title On the stabilization of the cylindrical precession of a satellite in an elliptic orbit
Author(s) I. A. Mukhametzyanov (Moscow)
Abstract In [1], a family of Lyapunov functions has been constructed for the stability analysis of unperturbed motions of time-varying systems on the basis of their linear approximation. In [2], this approach has been applied to construct mechanical systems having globally asymptotically stable design motions. In the present paper, these results are applied for the stabilization of the cylindrical precession of a satellite in an elliptic orbit. [This problem has been solved previously by S. A. Agafonov for a satellite moving in a circular orbit. See S. A. Agafonov, Stability Analysis of Motion of Nonconservative Mechanical Systems. A D.Sc. (Physics and Mathematics) Thesis [in Russian], MGU, Moscow, 1992.]
References
1.  I. A. Mukhametzyanov, "Construction of a family of Lyapunov functions," Vestnik RUDN. Ser. Prikl. Matematika i Informatika, No. 1, pp. 9-12, 1995.
2.  I. A. Mukhametzyanov, "Construction of systems with globally asymptotically stable design motions," Vestnik RUDN. Ser. Prikl. Matematika i Informatika, No. 1, pp. 16-21, 1998.
3.  V. V. Rumyantsev, "On the optimal stabilization of controlled systems," PMM [Applied Mathematics and Mechanics], Vol. 34, No. 3, pp. 440-456, 1970.
4.  N. N. Krasovskii, "Problems of stabilization of controlled motions," in I. G. Malkin, Theory of Stability of Motion [in Russian], Appendix 4, pp. 475-514, Nauka, Moscow, 1966.
5.  V. V. Beletskii, The Motion of a Satellite about its Center of Mass in the Gravitational Field [in Russian], Izd-vo MGU, Moscow, 1975.
6.  T. R. Kane and P. M. Barba, "Effects of energy dissipation on a spinning satellite," AIAA Journal, Vol. 4, No. 8, pp. 1391-1394, 1966.
Received 24 April 2000
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