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On the Stability of a Spinning Satellite in a Central Force Field

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Bifurcation and Chaos: Analysis, Algorithms, Applications

Abstract

It is known that the stability or instability of motion of a rigid axi-symmetric satellite spinning around its axis of symmetry can be determined by knowing its inertia-momentratio and its winding number [1,2]. This classical result is based on a linear stability analysis of the equation of motion which allows very small angular deviations of the satellite’s axis of symmetry from the space-fixed Z-direction (see Figure 1.).

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References

  1. Thomson, W.T.,“Spin Stabilization of Attitude against Gravity Torque”, Journal of the Astronautical Sciences, Vol. 9, No. 1, pp. 31–33, 1962.

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  2. Kane, T.R., Marsh, E.L., Wilson, W.G., “Letter to the Editor”, Journal of the Astronautical Sciences, Vol. 9, pp. 108–109, 1962.

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  3. Magnus, K., Kreisel, Springer-Verlag, Berlin, 1971.

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  4. Guran, A., Contributions to the Study of Instabilities in a Class of Conservative Systems, Toronto, 1990.

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  5. Richter, P.H., and Scholz, H.J. The Planar Double Pendulum, Film C1574, Göttingen; Publ. Wiss. Film, Sekt. Techn. Wiss/Naturw. Ser.9, Nr.7/C1574, 1985.

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© 1991 Birkhäuser Verlag Basel

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Guran, A. (1991). On the Stability of a Spinning Satellite in a Central Force Field. In: Seydel, R., Schneider, F.W., Küpper, T., Troger, H. (eds) Bifurcation and Chaos: Analysis, Algorithms, Applications. International Series of Numerical Mathematics / Internationale Schriftenreihe zur Numerischen Mathematik / Série Internationale d’Analyse Numérique, vol 97. Birkhäuser Basel. https://doi.org/10.1007/978-3-0348-7004-7_17

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  • DOI: https://doi.org/10.1007/978-3-0348-7004-7_17

  • Publisher Name: Birkhäuser Basel

  • Print ISBN: 978-3-0348-7006-1

  • Online ISBN: 978-3-0348-7004-7

  • eBook Packages: Springer Book Archive

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