DocumentCode :
3349434
Title :
Vector field guidance for three-dimensional curved path following with fixed-wing UAVs
Author :
Yueqian Liang ; Yingmin Jia ; Junping Du ; Jun Zhang
Author_Institution :
Seventh Res. Div. & the Center for Inf. & Control, Beihang Univ. (BUAA), Beijing, China
fYear :
2015
fDate :
1-3 July 2015
Firstpage :
1187
Lastpage :
1192
Abstract :
This paper investigates the three-dimensional (3D) curved path following problem using fixed-wing unmanned aerial vehicles (UAVs) in the presence of constant wind disturbance. Vector field based approaches are used as the solution. Two vector fields are first developed, one is the tangent vector field based on path tangent vector and coordinate transformation, and the other is the combined vector field based on the combination of a conservative vector field and a solenoidal vector field. A unified jointly saturated course rate and saturated climb rate controller is designed based on the proposed vector fields. Simulations are conducted to demonstrate the effectiveness of the proposed approach.
Keywords :
autonomous aerial vehicles; position control; simulation; vectors; conservative vector field; coordinate transformation; fixed-wing UAV; fixed-wing unmanned aerial vehicles; path tangent vector; simulations; solenoidal vector field; three-dimensional curved path following problem; vector field guidance; wind disturbance; Convergence; Electronic mail; Kinematics; Mathematical model; Target tracking; Three-dimensional displays; Trajectory;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
American Control Conference (ACC), 2015
Conference_Location :
Chicago, IL
Print_ISBN :
978-1-4799-8685-9
Type :
conf
DOI :
10.1109/ACC.2015.7170894
Filename :
7170894
Link To Document :
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