An intelligent missile autopilot using genetic algorithm

Author

Kim, Yoon-Sik ; Han, Woong-Gie ; Kuc, Tae-Yong

Author_Institution

Intelligent Control & Dynamic Simulation Lab., Sung Kyun Kwan Univ., Suwon, South Korea

Volume

2

fYear

1997

fDate

12-15 Oct 1997

Firstpage

1954

Abstract

This paper presents an intelligent autopilot for STT missiles with multiple controllers. The mixed H₂/H_∞ control technique is applied for each controller and implemented by using the genetic searching algorithm. To facilitate automatic switching of multiple controllers under different operating conditions, an error based switching scheme is also combined with the intelligent control system. It is shown via computer simulation that the proposed autopilot outperforms the conventional one

Keywords

H^∞ control; genetic algorithms; intelligent control; missile control; search problems; STT missiles; automatic switching; error based switching scheme; genetic searching algorithm; intelligent missile autopilot; mixed H₂/H_∞ control technique; multiple controllers; Aerodynamics; Automatic control; Control systems; Error correction; Genetic algorithms; Intelligent control; Missiles; Neural networks; Nonlinear dynamical systems; Optimal control;

fLanguage

English

Publisher

ieee

Conference_Titel

Systems, Man, and Cybernetics, 1997. Computational Cybernetics and Simulation., 1997 IEEE International Conference on

Conference_Location

Orlando, FL

ISSN

1062-922X

Print_ISBN

0-7803-4053-1

Type

conf

DOI

10.1109/ICSMC.1997.638363

Filename

638363