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Adaptative control for bioinspired micro air vehicles

Publicado en:8th Conference On Smart Structures And Materials, Smart 2017 And 6th International Conference On Smart Materials And Nanotechnology In Engineering, Smn 2017. 2017-January 400-411 - 2017-01-01 2017-January(), DOI:

Autores: Crespo-Moreno J; Barcala-Montejano M; Rodríguez-Sevillano Á; Alonso-Alarcón J; Bardera-Mora R; Shportenko D; Romero-García A

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© 2017 International Center for Numerical Methods in Engineering. All rights reserved. The amazing world of drones supposes a field of aerospace research really exciting for universities and centers of excellence, and practically without technological limitations. Perhaps the reality is that the use of these drones is less glamorous than the media suggest. And, on the other hand, its operations are still limited by pending aspects of aeronautical regulation. But in the field of aerospace research the previous arguments are weak compared to the potential of new aerospace designs and developments. The authors have been carrying out several research projects in the field of micro air vehicles. In addition, last researches have been outstanding in the analysis of bioinspired micro air vehicles (MAVs). Experimental and theoretical studies have been developed and aircraft prototypes based on morphing wings and wing-grids have been designed. For the design of this type of non-conventional geometry it is essential to select the appropriate materials that will meet the initial design specifications. And when the geometry and materials are finally defined, the next essential step is the design of the wing geometry control system. This system will allow to fulfilling the flight requirements. This paper shows the methodology of design for the flight control system carried out on these vehicles. The initial basis begins from our development in traditional flight control for guidance, navigation and control systems in conventional geometry airplanes. Subsequently, the foundations of adaptive and optimal control will be shown. Finally, the results of flight control over micro air vehicles' prototypes will be analyzed in the current design phase.

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