DESIGN OF ADAPTIVE OUTPUT FEEDBACK CONTROLLER BASED ON HIGH-ORDER SLIDE OBSERVER FOR MISSILE LAUNCHERS

Abstract

The controller of the launcher drive system plays a very important role in
stabilizing the control quality and increasing the probability of destroying the
target. This paper presents the results of building an adaptive output feedback
controller based on a high-order sliding observer for the CM-90 launcher drive
system of the C-75-M3 air defense missile system. The simulation test results
on Matlab-Simulink software show that this controller ensures control
accuracy; stabilizes the system even when there is strong interference.