On bounded satellite motion under constant radial propulsive acceleration
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Universidad de La Rioja
info
- 2 Columnas de Hercules 1, 11100 San Fernando, Spain
ISSN: 1024-123X
Year of publication: 2012
Volume: 2012
Pages: 1-13
Type: Article
More publications in: Mathematical Problems in Engineering
Abstract
The Hamiltonian formulation of the constant radial propulsive acceleration problem in nondimensional units reveals that the problem does not depend on any physical parameter. The qualitative description of the integrable flow is given in terms of the energy and the angular momentum, showing that the different regimes are the result of a bifurcation phenomenon. The solution via the Hamilton-Jacobi equation demonstrates that the elliptic integrals of the three kinds are intrinsic to the problem. © 2012 Juan F. San-Juan et al.