Trajectory tracking of a satellite communicated missile with Fuzzy and PID control

Author

Yagimli, Mustafa ; Simsir, Ugur ; Tozan, Hakan

Author_Institution

Marmara Univ., Istanbul, Turkey

fYear

2011

fDate

9-11 June 2011

Firstpage

318

Lastpage

323

Abstract

In this study, the trajectory of a satellite communicated missile, which is thrown from combat plane to combat plane, has been investigated with using Fuzzy and PID control separately. The Guidance Section of Missile consists of an active radar seeker and radome, radar altimeter and antennas, and power converter. Simulations have been done with Matlab Simulink toolbox and utilized standard transfer function of missile on block diagram. The results, enabled with PID and Fuzzy Control, have been compared and given in this study.

Keywords

fuzzy control; missile guidance; object tracking; position control; radar altimetry; radar antennas; radar tracking; radomes; satellite communication; three-term control; transfer functions; Matlab Simulink toolbox; PID control; active radar; combat plane; fuzzy control; guidance section of missile; power converter; radar altimeter; radar antenna; satellite communicated missile; trajectory tracking; transfer function; Education; Missiles; Yttrium; PID control; fuzzy control; missile; trajectory tracking;

fLanguage

English

Publisher

ieee

Conference_Titel

Recent Advances in Space Technologies (RAST), 2011 5th International Conference on

Conference_Location

Istanbul

Print_ISBN

978-1-4244-9617-4

Type

conf

DOI

10.1109/RAST.2011.5966848

Filename

5966848