2009
DOI: 10.1515/forum.2009.038
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Geodesic flow of the averaged controlled Kepler equation

Abstract: A normal form of the Riemannian metric arising when averaging the coplanar controlled Kepler equation is given. This metric is parameterized by two scalar invariants which encode its main properties. The restriction of the metric to S 2 is shown to be conformal to the flat metric on an oblate ellipsoid of revolution, and the associated conjugate locus is observed to be a deformation of the standard astroid. Though not complete because of a singularity at the origin in the space of ellipses, the metric has conv… Show more

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Cited by 15 publications
(25 citation statements)
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“…The authors prove that it is possible to follow a path of solutions starting from λ = 0 and reaching a value of λ very close to 1, which permits then to initialize successfully the shooting method with λ = 1. It can be noted that the heuristics t f T max Cst has been understood and clearly explained in the papers [182,183]. In these references, based on preliminary results of [184] where the optimal trajectories of the energy minimization problem are approximated using averaging techniques, the averaged Hamiltonian system is explicitly computed and is shown to be a Riemannian problem.…”
Section: Application To the Orbit Transfer Problem With Low Thrustmentioning
confidence: 99%
“…The authors prove that it is possible to follow a path of solutions starting from λ = 0 and reaching a value of λ very close to 1, which permits then to initialize successfully the shooting method with λ = 1. It can be noted that the heuristics t f T max Cst has been understood and clearly explained in the papers [182,183]. In these references, based on preliminary results of [184] where the optimal trajectories of the energy minimization problem are approximated using averaging techniques, the averaged Hamiltonian system is explicitly computed and is shown to be a Riemannian problem.…”
Section: Application To the Orbit Transfer Problem With Low Thrustmentioning
confidence: 99%
“…The case p φ (0) = 0 corresponds for an initial condition not on the equator to tangential arrival and departure at parallels φ(0) and π − φ(0); p φ (0) = 0 gives the equator solution in the non singular case. For more details see [5].…”
Section: Geometric Propertiesmentioning
confidence: 99%
“…The study of them and the resurgence of their significance has not been visible since the notorious and colossal triptych of Breiter [1][2][3]. Later rebranded by Rossi [4] in the context of the medium-Earth orbits (MEOs), the study of their long-term dynamics, and in particular their eccentricity growths in the elliptic domain [5], represent current deep motivations for the community. In our opinion, the most complete and up-to-date panorama of the literature is excellently presented by Armellin and San-Juan [6].…”
Section: Introductionmentioning
confidence: 99%