Title :
Nonlinear controllers for a tail-fin controlled missile
Author :
Serakos, Demetrios
Author_Institution :
US Naval Surface Warfare Center, Dahlgren, VA, USA
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;
Conference_Titel :
Southeastcon '93, Proceedings., IEEE
Conference_Location :
Charlotte, NC
Print_ISBN :
0-7803-1257-0
DOI :
10.1109/SECON.1993.465725
