SYNTHESIS OF SLIDING CONTROLLER ON BASIS LINEAR MATRIX INEQUALITIES FOR AIR-ROD DRIVE SYSTEM

Abstract

The paper presents the results of constructing finite time sliding controller
on the basis of Linear Matrix Inequalities (LMI) for 57mm anti-aircraft gun drive
system. The simulation test results on Matlab-Simulink software show that this
controller ensures the grip accuracy; stabilize engine speed, load; eliminates
vibrations under system conditions influenced by nonlinear factors caused by
mechanical structure and firing impulses.