ISSN 2079-8490

Electronic scientific journal "Scientists notes PNU"

Pacific national university

Kupriyanova О. V., Lelyanov B.N.


A mathematical model of the automatic control system X-wing missile. Driven model SAUunder the influence of external disturbances made using MatLAB Simulink. Produced stabilization of the system and its analysis on the basis of timing charts.

Keywords: simulation, MatLAB, riskov, roll, pitch, X-wing rocket.