DocumentCode :
3496331
Title :
An overview of aerial refueling control systems applied to UAVs
Author :
Panday, A. ; Pedro, Jimoh O.
Author_Institution :
Sch. of Mech., Ind. & Aeronaut. Eng., Univ. of the Witwatersrand, Johannesburg, South Africa
fYear :
2013
fDate :
9-12 Sept. 2013
Firstpage :
1
Lastpage :
5
Abstract :
The development and extension of unmanned aerial vehicle (UAV) capabilities has ignited a renewed interest in aerial refueling. Two methods of aerial refueling still remain: boom-receptacle and probe-drogue. The receiver aircraft dynamics are complex, nonlinear and cross-coupled to that of the tanker, causing relative control to be a challenge. A survey of flight control systems as applied to the problem of UAV aerial refueling has been performed. Various techniques, both classical and novel, have been applied to this control problem. Trends indicate a focused research effort within specific aspects of aerial refueling. Even with much attention being given to this field, control system designs have by no means been exhausted.
Keywords :
aircraft control; autonomous aerial vehicles; control system synthesis; fuel systems; UAV; aerial refueling control system; boom-receptacle; control system design; flight control system; probe-drogue; receiver aircraft dynamics; tanker; unmanned aerial vehicle; Aerodynamics; Aerospace control; Aircraft; Atmospheric modeling; Control systems; Military aircraft; Receivers; aerial refueling; control systems; unmanned aerial vehicle (UAV); unmanned combat aerial vehicle (UCAV);
fLanguage :
English
Publisher :
ieee
Conference_Titel :
AFRICON, 2013
Conference_Location :
Pointe-Aux-Piments
ISSN :
2153-0025
Print_ISBN :
978-1-4673-5940-5
Type :
conf
DOI :
10.1109/AFRCON.2013.6757788
Filename :
6757788
Link To Document :
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