IAM 02674
INSTITUTO ARGENTINO DE MATEMATICA ALBERTO CALDERON
Unidad Ejecutora - UE
congresos y reuniones científicas
Título:
Fault tolerant control of an hexacopter with a tilted-rotor configuration
Autor/es:
POSE CLAUDIO; IGNACIO MAS; GIRIBET JUAN
Lugar:
Mar del Plata
Reunión:
Congreso; XVII Reunión de trabajo en Procesamiento de la Información y Control; 2017
Institución organizadora:
RPIC
Resumen:
Recently, it was shown that an hexagon-shapedhexa-rotor micro aerial vehicle with unidirectionally spinningtilted rotors is capable of fault tolerant attitude and altitudecontrol. This result has been theoretically proven and validatedby simulations. However, experimental results have never beenreported yet. In this work experimental results are presented,and a comparison between a tilted-rotor hexacopter with one ina standard rotor configuration is carried out.
