A technique for aircraft control system design using MATLAB/Simulink software

Аuthors

Matveyev A. V.^*, Bobronnikov V. Т.^**

Moscow Aviation Institute (National Research University), 4, Volokolamskoe shosse, Moscow, А-80, GSP-3, 125993, Russia

*e-mail: Anatolii_84@mail.ru
**e-mail: vlbobronnikov@yandex.ru

Abstract

A technique is presented to design control systems for unmanned aerial vehicles (UAV). The technique suggests a step-by-step automated synthesis including solving of optimization problems for controllers basing on transient performance criteria within a space of tuned parameters. An example is described to demonstrate an application of the technique for control system synthesis in regard to a gliding UAV.

Keywords:

control system, aircraft, motion modeling