Nonlinear controllers for a tail-fin controlled missile

30 December 2002

conference paper
Published by Institute of Electrical and Electronics Engineers (IEEE)

p. 8 p.
https://doi.org/10.1109/secon.1993.465725

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

MISSILES
AERODYNAMICS
EQUATIONS
FORCE CONTROL
ANGULAR VELOCITY CONTROL
PRESSURE CONTROL
WEIGHT CONTROL
ACCELERATION
ACTUATORS
ELECTRONIC SWITCHING SYSTEMS

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