Abstract
Two sufficient conditions for the existence of the Jacobian constant in the restricted circular three body problem, when the satellite body is a gyrostat, are given. In both conditions, the analytical expression of Jacobian constant is found. The rigid body and the classical cases are obtained as particular solutions.
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© 1986 D. Reidel Publishing Company
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Elipe, A., Arribas, M. (1986). An Extension of Jacobian Constant. In: Bhatnagar, K.B. (eds) Space Dynamics and Celestial Mechanics. Astrophysics and Space Science Library, vol 127. Springer, Dordrecht. https://doi.org/10.1007/978-94-009-4732-0_5
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DOI: https://doi.org/10.1007/978-94-009-4732-0_5
Publisher Name: Springer, Dordrecht
Print ISBN: 978-94-010-8603-5
Online ISBN: 978-94-009-4732-0
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