THE REASEARCHOF CONTROL SYSTEM OFANGULAR POSITION OF UNMANNED AERIAL VEHICLE

Abstract

The results of the control system of unmanned aircraft in the channel longitudinal motion (pitch angle control). A system has been studied with actuator with rigid feedback, speed feedback and izodromic feedback when changing the coefficients of the angular velocity sensor and the angle sensor. The research of system of control was performed in the graphical modeling environment Simulink Matlab package. Based on the results of computer simulation was proposed optimal variant of the actuator feedback.