SYNTHESIS OF SLIDING CONTROLLER ON BASIS LINER QUADRATIC REGULATOR FOR AIR-ROD DRIVE SYSTEM

Abstract

The aircraft altitude control channel plays a very important role in stabilizing
the flight path. This paper presents the results of building a liner quadratic
regulator controller for the elevation channel. The test results by simulation on
Matlab-Simulink software show that this controller ensures tracking accuracy;
stable altitude even in the presence of strong noise.