Hybrid Optimal Control Approach to Commercial Aircraft Trayectory Planning

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Hybrid Optimal Control Approach to Commercial Aircraft Trayectory Planning

Author(s): Soler, Manuel; Olivares, Alberto; Staffetti, Ernesto
Publisher: American Institute of Aeronautics and Astronautics, Inc.
Issued date: 2010-05
Citation: Journal of Guidance, Control, and Dynamics (2013). 33(3), 985-991.
ISSN: 0731-5090 (print)
1533-3884 (online)
DOI: 10.2514/1.47458
Sponsor: This work is partially supported by the Spanish Government through the Ministerio de Ciencia e Innovación, the Comunidad de Madrid, and the project i-Math Ingenio Mathematica. This work has been carried out within the framework of the Atlantida project, partially funded by the Spanish Centro para el Desarrollo Tecnológico e Industrial, in which the Universidad Rey Juan Carlos is collaborating with GVM Aerospace and Defence.
Publisher version: http://dx.doi.org/10.2514/1.47458
Keywords: Optimal Control , Hybrid Systems , Aircraft Operations , Aircraft Trajectory Planning
URI: http://hdl.handle.net/10016/20907
Rights: © 2010 American Institute of Aeronautics and Astronautics, Inc.

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