Geometric optimal control of elliptic Keplerian orbits - Archive ouverte HAL
Article Dans Une Revue Discrete and Continuous Dynamical Systems - Series S Année : 2005

Geometric optimal control of elliptic Keplerian orbits

Résumé

This article deals with the transfer of a satellite between Keplerian orbits. We study the controllability properties of the system and make a preliminary analysis of the time optimal control using the maximum principle. Second order sufficient conditions are also given. Finally, the time optimal trajectory to transfer the system from an initial low orbit with large eccentricity to a terminal geostationary orbit is obtained numerically.
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Dates et versions

hal-00086345 , version 1 (18-07-2006)

Identifiants

  • HAL Id : hal-00086345 , version 1

Citer

Bernard Bonnard, Jean-Baptiste Caillau, Emmanuel Trélat. Geometric optimal control of elliptic Keplerian orbits. Discrete and Continuous Dynamical Systems - Series S, 2005, Series B, 5 (4), pp.929--956. ⟨hal-00086345⟩
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