Editorial:
American Institute of Aeronautics and Astronautics, Inc.
Fecha de edición:
2010-05
Cita:
Journal of Guidance, Control, and Dynamics (2013). 33(3), 985-991.
ISSN:
0731-5090 (print) 1533-3884 (online)
DOI:
10.2514/1.47458
Agradecimientos:
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.
