학술논문

Adaptive Neural Network Controller Design for Missile Systems with Unmodeled Dynamics
Document Type
Conference
Source
The Proceedings of the Multiconference on "Computational Engineering in Systems Applications" Computational Engineering in Systems Applications, IMACS Multiconference on. 1:789-793 Oct, 2006
Subject
Computing and Processing
Components, Circuits, Devices and Systems
Adaptive systems
Programmable control
Adaptive control
Neural networks
Control systems
Missiles
Design methodology
Nonlinear systems
Nonlinear dynamical systems
Backstepping
Input unmodeled dynamics
nonlinear systems
backstepping
adaptive inverse
Language
Abstract
An adaptive inverse compensator design method was proposed for a class of nonlinear systems with input ummodeled dynamics based on RBF neural networks. The compensator was designed using two neural networks, one to estimate the input unmodeled dynamics and another to provide adaptive inverse compensation to the input unmodeled dynamics. The method relaxes some rigorous demands to unmodeled dynamics such as relative degree zero, satisfying the small gain assumption and so on. The controller was designed using backstepping control techniques. Lyapunov theory was used to derive the tuning laws for the weight vectors of the neural networks and proved that the close-loop system is gradually stable. The proposed method is applied to design the missile control systems with input unmodeled dynamics in pitch channel. The simulation results show the effectiveness of the proposed control method.