Geometric Orbital Transfer Using Averaging Techniques

Geometric Orbital Transfer Using Averaging Techniques

In this article, we focus on the coplanar orbital transfer of a satellite between Keplerian orbits, with low propulsion. We compute and analyze averaged systems associated with the energy minimization problem with the full control or control oriented in a single direction, tangential-normal or radia...

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Veröffentlicht in:Journal of dynamical and control systems 2008-04, Vol.14 (2), p.145-167
Hauptverfasser: Bonnard, B., Janin, G.
Format: Artikel
Sprache:eng
Schlagworte:
Calculus of Variations and Optimal Control
Optimization
Control
Control systems
Dynamical Systems
Dynamical Systems and Ergodic Theory
Dynamics
Energy conservation
Mathematics
Mathematics and Statistics
Optimization
Orbitals
Orbits
Satellites
Systems Theory
Vibration
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Beschreibung
Zusammenfassung:In this article, we focus on the coplanar orbital transfer of a satellite between Keplerian orbits, with low propulsion. We compute and analyze averaged systems associated with the energy minimization problem with the full control or control oriented in a single direction, tangential-normal or radial-orthoradial. This allows to understand the properties of each control direction in the optimal control problems.
ISSN:1079-2724
1573-8698
DOI:10.1007/s10883-008-9040-1