DocumentCode
3428332
Title
Neural network-based optimal control for trajectory tracking of a helicopter UAV
Author
Nodland, David ; Zargarzadeh, H. ; Jagannathan, S.
Author_Institution
Dept. of Electr. & Comput. Eng., Missouri Univ. of Sci. & Technol., Rolla, MO, USA
fYear
2011
fDate
12-15 Dec. 2011
Firstpage
3876
Lastpage
3881
Abstract
Helicopter unmanned aerial vehicles (UAVs) may be widely used for both military and civilian operations. Because these helicopters are underactuated nonlinear mechanical systems, high-performance controller design for them presents a challenge. This paper presents an optimal controller design for trajectory tracking of a helicopter UAV using a neural network (NN). The state-feedback control system utilizes the backstepping methodology, employing kinematic and dynamic controllers. The online approximator-based dynamic controller learns the infinite-horizon Hamilton-Jacobi-Bellman (HJB) equation in continuous time and calculates the corresponding optimal control input to minimize the HJB equation forward-in-time. Optimal tracking is accomplished with a single NN utilized for cost function approximation. The overall closed-loop system stability is demonstrated using Lyapunov analysis, with the position, orientation, angular and translational velocity tracking errors, and NN weight estimation errors uniformly ultimately bounded (UUB) in the presence of bounded disturbances and NN functional reconstruction errors.
Keywords
Lyapunov methods; aerospace robotics; angular velocity control; approximation theory; autonomous aerial vehicles; closed loop systems; control system synthesis; helicopters; mobile robots; neurocontrollers; nonlinear control systems; optimal control; position control; robot dynamics; robot kinematics; stability; state feedback; HJB equation; Lyapunov analysis; NN functional reconstruction error; NN weight estimation error; angular velocity tracking error; backstepping methodology; civilian operation; closed-loop system stability; cost function approximation; dynamic controller; helicopter UAV; high-performance controller design; infinite-horizon Hamilton-Jacobi-Bellman equation; kinematic controller; military operation; neural network-based optimal control; online approximator-based dynamic controller; orientation tracking error; position tracking error; state-feedback control system; trajectory tracking; translational velocity tracking error; underactuated nonlinear mechanical systems; uniformly ultimately bounded; unmanned aerial vehicles; Artificial neural networks; Cost function; Equations; Helicopters; Mathematical model; Optimal control; Vectors;
fLanguage
English
Publisher
ieee
Conference_Titel
Decision and Control and European Control Conference (CDC-ECC), 2011 50th IEEE Conference on
Conference_Location
Orlando, FL
ISSN
0743-1546
Print_ISBN
978-1-61284-800-6
Electronic_ISBN
0743-1546
Type
conf
DOI
10.1109/CDC.2011.6160554
Filename
6160554
Link To Document