Abstract
This article deals with the optimal transfer of a satellite between Keplerian orbits when the control is oriented along the tangential direction. We consider the time-optimal control problem and the energy minimization problem. The optimal controls laws have discontinuities and continuations and averaging techniques are applied to smooth the discontinuities. The smooth approximations of the solutions are computed using a shooting method taking into account second-order optimality conditions.
Original language | English |
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Title of host publication | Taming Heterogeneity and Complexity of Embedded Control |
Subtitle of host publication | Selected papers presented at the Joint CTS-HYCON Workshop on Nonlinear and Hybrid Control, Paris IV Sorbonne, 10-12 July 2006 |
Editors | Francoise LAMNABHI-LAGARRIGUE, Salah LAGHROUCHE, Antonio LORIA, Elena PANTELEY |
Place of Publication | Londres |
Publisher | International Scientific and Technical Encyclopaedia |
Pages | 73-96 |
Number of pages | 24 |
Publication status | Published - 2006 |
Keywords
- shooting method
- continuation method
- second-order optimality condition
- single-input orbit transfer
- averaging
- Optimal control