Aerospace Instrument-Making Annotation << Back Aircraft control system design in matlab / simulink software A.V. Matveyev, V.T. Bobronnikov It is presented unmanned aerial vehicle control system design method. Method offers automated step-by-step synthesis including compensators optimization solutions in terms of quality step response criterion through functional extremum seeking in tune parameters space. Method allows to automate and streamline control design. An example of method application for gliding aircraft control system design is provided. Key words: Control system, aircraft, motion modeling. E-mail: Anatolii_84@mail.ru