DocumentCode :
2736573
Title :
Flight safety improvements for small size unmanned aerial vehicles
Author :
Stojcsics, D.
Author_Institution :
Doctoral Sch. of Appl. Inf., Obuda Univ., Budapest, Hungary
fYear :
2012
fDate :
13-15 June 2012
Firstpage :
483
Lastpage :
487
Abstract :
Unmanned aerial vehicles from micro to large scale are a common research topic in the latest years. Small size (under 3 m wingspan and between 1-15 kg all up weight) UAVs and the autopilots usually have no redundancy and have been not prepared for emergency situations. Loss of control, power management, engine or a faulty sensor could cause serious damage. To prevent the disaster many things must be considered and added to the UAV such as redundant manual and autonomous controller, fault detection and isolation subsystem (FDI) or bearing and position estimation. The AERObot autopilot was developed at Obuda University for research purposes using multiple flight safety improvement methods.
Keywords :
aerospace safety; autonomous aerial vehicles; disasters; fault diagnosis; mobile robots; position control; AERObot autopilot; FDI; Obuda University; UAV; autonomous controller; bearing estimation; disaster prevention; emergency situation; fault detection-and-isolation subsystem; flight safety improvement; mass 1 kg to 15 kg; position estimation; redundant manual controller; size 3 m; small size unmanned aerial vehicle; Actuators; Conferences; Elevators; Estimation; Global Positioning System; Manuals;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Intelligent Engineering Systems (INES), 2012 IEEE 16th International Conference on
Conference_Location :
Lisbon
Print_ISBN :
978-1-4673-2694-0
Electronic_ISBN :
978-1-4673-2693-3
Type :
conf
DOI :
10.1109/INES.2012.6249882
Filename :
6249882
Link To Document :
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