Wing Missiles Stabilization Based on Sliding Mode Control

24 August 2005

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

p. 574-578
https://doi.org/10.1109/aerocs.1993.720999

Abstract

The problem of developing of the accuracy of the platform stabilization with "passengers" placed on the wing missiles is considered. The special approach to the stabilization problem solution based on sliding modes has been developed. The problem of high precision stabilization of the platform with sensor based on dynamically tuned gyroscope has been solved.

Keywords

MISSILES
SLIDING MODE CONTROL
GYROSCOPES
DIFFERENTIAL EQUATIONS
CONTROL SYSTEMS
DIFFERENTIAL ALGEBRAIC EQUATIONS
SWITCHES
MATHEMATICS
CITIES AND TOWNS
ACCELEROMETERS

This publication has 2 references indexed in Scilit:

Variable structure control of nonlinear multivariable systems: a tutorial
Proceedings of the IEEE, 1988
Variable structure systems with sliding modes
IEEE Transactions on Automatic Control, 1977