DocumentCode
3184381
Title
Nonlinear controllers for a tail-fin controlled missile
Author
Serakos, Demetrios
Author_Institution
US Naval Surface Warfare Center, Dahlgren, VA, USA
fYear
1993
fDate
4-7 Apr 1993
Firstpage
0.833333333333333
Abstract
Several distinct nonlinear controllers are applied to the nonlinear pitch plane dynamics of a tail-fin controlled missile. The nonlinear controllers are assessed via simulation studies for performance and robustness to plant parameter variations. Numerical examples are presented to illustrate the controllers
Keywords
controllers; missile control; nonlinear control systems; nonlinear controllers; nonlinear pitch plane dynamics; performance analysis; plant parameter variations; robustness; simulation studies; tail-fin controlled missile; Acceleration; Actuators; Aerodynamics; Angular velocity control; Electronic switching systems; Equations; Force control; Missiles; Pressure control; Weight control;
fLanguage
English
Publisher
ieee
Conference_Titel
Southeastcon '93, Proceedings., IEEE
Conference_Location
Charlotte, NC
Print_ISBN
0-7803-1257-0
Type
conf
DOI
10.1109/SECON.1993.465725
Filename
465725
Link To Document