Title :
Neural Network-Based Optimal Adaptive Output Feedback Control of a Helicopter UAV
Author :
Nodland, D. ; Zargarzadeh, H. ; Jagannathan, Sarangapani
Author_Institution :
Dept. of Electr. & Comput. Eng., Missouri Univ. of Sci. & Technol., Rolla, MO, USA
Abstract :
Helicopter unmanned aerial vehicles (UAVs) are widely used for both military and civilian operations. Because the helicopter UAVs are underactuated nonlinear mechanical systems, high-performance controller design for them presents a challenge. This paper introduces an optimal controller design via an output feedback for trajectory tracking of a helicopter UAV, using a neural network (NN). The output-feedback control system utilizes the backstepping methodology, employing kinematic and dynamic controllers and an NN observer. The online approximator-based dynamic controller learns the infinite-horizon Hamilton-Jacobi-Bellman equation in continuous time and calculates the corresponding optimal control input by minimizing a cost function, forward-in-time, without using the value and policy iterations. Optimal tracking is accomplished by using a single NN utilized for the cost function approximation. The overall closed-loop system stability is demonstrated using Lyapunov analysis. Finally, simulation results are provided to demonstrate the effectiveness of the proposed control design for trajectory tracking.
Keywords :
Lyapunov methods; adaptive control; autonomous aerial vehicles; closed loop systems; continuous time systems; control system synthesis; feedback; helicopters; neurocontrollers; nonlinear systems; observers; optimal control; stability; trajectory control; Lyapunov analysis; NN observer; backstepping methodology; civilian operations; closed-loop system stability; continuous time; dynamic controllers; forward-in-time; helicopter UAV; helicopter unmanned aerial vehicles; high-performance controller design; infinite-horizon Hamilton-Jacobi-Bellman equation; kinematic controllers; military operations; neural network-based optimal adaptive output feedback control; online approximator-based dynamic controller; optimal controller design; optimal tracking; trajectory tracking; underactuated nonlinear mechanical systems; Hamilton–Jacobi–Bellman (HJB) equation; helicopter unmanned aerial vehicle (UAV); neural network (NN); nonlinear optimal control;
Journal_Title :
Neural Networks and Learning Systems, IEEE Transactions on
DOI :
10.1109/TNNLS.2013.2251747