Optimal Hybrid Control of a Gyroscope System

Abstract

The paper analyses the selection of optimal controllers (LQR, SMC and PD) for a mechatronic gyroscope system used in scanning-tracking heads of mobile objects such as spacecrafts, unmanned land vehicles, flying drones or self-guided missiles. The integral of the absolute value of the deviation error of the set motion from the real moving object and the integral of the square of the state and control have been taken as the quality criterion. The results of computer simulation studies are presented.