DocumentCode :
104240
Title :
Fixed Wing UAV Path Following in Wind With Input Constraints
Author :
Beard, R.W. ; Ferrin, Jeff ; Humpherys, Jeffrey
Author_Institution :
Electr. & Comput. Eng. Dept., Brigham Young Univ., Provo, UT, USA
Volume :
22
Issue :
6
fYear :
2014
fDate :
Nov. 2014
Firstpage :
2103
Lastpage :
2117
Abstract :
This paper considers the problem of fixed wing unmanned air vehicles following straight lines and orbits. To account for ambient winds, we use a path following approach as opposed to trajectory tracking. The unique feature of this paper is that we explicitly account for roll and flight path angle constraints. The guidance laws are derived using the theory of nested saturations, and explicit flight conditions are derived that guarantee convergence to the path. The method is validated by simulation and flight tests.
Keywords :
aerospace components; aerospace simulation; aircraft testing; autonomous aerial vehicles; path planning; wind; ambient winds; explicit flight conditions; fixed wing UAV path following; fixed wing unmanned air vehicles; flight path angle constraints; flight test; guidance laws; input constraints; nested saturation theory; roll angle constraints; simulation; trajectory tracking; Kinematics; Motion planning; Nonlinear control systems; Orbits; Unmanned aerial vehicles; Aircraft Navigation; motion planning; nonlinear control systems; unmanned systems; unmanned systems.;
fLanguage :
English
Journal_Title :
Control Systems Technology, IEEE Transactions on
Publisher :
ieee
ISSN :
1063-6536
Type :
jour
DOI :
10.1109/TCST.2014.2303787
Filename :
6740857
Link To Document :
بازگشت