DocumentCode
335429
Title
Performance enhancement of a missile autopilot via genetic algorithm optimization techniques
Author
Hull, Richard A. ; Johnson, Roger W.
Author_Institution
Inst. for Simulation & Training, Central Florida Univ., Orlando, FL, USA
Volume
2
fYear
1994
fDate
29 June-1 July 1994
Firstpage
1680
Abstract
The objective of this study is to demonstrate that genetic algorithm optimisation techniques can be successfully applied to enhance the performance of a typical linear quadratic missile autopilot controller design by incorporating several combinations of performance goals and constraints.
Keywords
genetic algorithms; linear quadratic control; missile guidance; navigation; LQ controller; genetic algorithm; linear quadratic control; missile autopilot; optimal control; optimization; performance enhancement; Aerodynamics; Algorithm design and analysis; Control systems; Design optimization; Feedback control; Genetic algorithms; Hydraulic actuators; Missiles; Robust stability; System performance;
fLanguage
English
Publisher
ieee
Conference_Titel
American Control Conference, 1994
Print_ISBN
0-7803-1783-1
Type
conf
DOI
10.1109/ACC.1994.752357
Filename
752357
Link To Document