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