Title :
Quadrotors flight formation control using a leader-follower approach
Author :
Mercado, D.A. ; Castro, R. ; Lozano, Rogelio
Author_Institution :
Dept. of Electr. Eng., CINVESTAV-IPN, Mexico City, Mexico
Abstract :
In this paper it is presented a control strategy to solve the trajectory tracking and flight formation problem, in horizontal plane, of multiple unmanned aerial vehicles (UAVs) kind quadrotor, by means of a leader-follower scheme. Time scale separation of the translational and rotational quadrotor dynamics is used to achieve trajectory tracking. A sliding mode controller is proposed for the translational dynamic and provides the desired orientation for the UAV, which is controlled by a linear PD control. Finally, from the formation error dynamics, a sliding mode control is used by the follower to preserve the formation with respect to a leader. Experimental results, using a virtual leader and a follower in formation, are shown to evaluate the proposed control law.
Keywords :
PD control; aircraft control; autonomous aerial vehicles; helicopters; linear systems; variable structure systems; vehicle dynamics; control law; flight formation problem; formation error dynamics; horizontal plane; leader-follower approach; linear PD control; multiple unmanned aerial vehicles; quadrotor flight formation control; rotational quadrotor dynamics; sliding mode controller; time scale separation; trajectory tracking; translational quadrotor dynamics; Attitude control; Equations; Lead; Trajectory; Uncertainty; Vectors; Vehicle dynamics;
Conference_Titel :
Control Conference (ECC), 2013 European
Conference_Location :
Zurich