Design of robust systems for the stabilization of unmanned aircraft equipment


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Abstract

A model of a triaxial system for the stabilization and control of sight axis orientation of observation devices operated at unmanned aircraft is developed. The features of the robust structural synthesis procedure as applied to a system of the type analyzed are discussed. The results of the simulation of a synthesized system are presented.

About the authors

O. A. Sushchenko

National Aviation University

Author for correspondence.
Email: sushoa@ukr.net

Candidate of Science (Enfinering)

Professor of the Aircraft Control Systems Department

Ukraine

V. N. Azarskov

National Aviation University

Email: azarskov@nau.edu.ua

Doctor of Science (Engineering)

Head of the Aircraft Control Systems Department

Ukraine

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