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