<abstract xmlns="http://www.w3.org/1999/xhtml"><p>This article deals with robust <italic>H</italic>∞ optimal control of the flight control systems of the small unmanned aerial vehicles (UAVs) in the presence of the plant disturbances and sensor noises. The rationales of the theory of <italic>H</italic>∞ controller synthesis are brought into a unique frame supporting design procedures being implemented. The paper focuses on numerical example of the synthesis of the controller of the flight control system of the small UAV.</p></abstract>

This article deals with robust H∞ optimal control of the flight control systems of the small unmanned aerial vehicles (UAVs) in the presence of the plant disturbances and sensor noises. The rationales of the theory of H∞ controller synthesis are brought into a unique frame supporting design procedures being implemented. The paper focuses on numerical example of the synthesis of the controller of the flight control system of the small UAV.

Robust <italic>H</italic>∞ Optimal Controller Design for The Small Unmanned Aerial Vehicle

Land Forces Academy Review

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Robust ∞ Optimal Controller Design for The Small Unmanned Aerial Vehicle

This article deals with robust H∞ optimal control of the flight control systems of the small unmanned aerial vehicles (UAVs) in the presence of the plant...

Robust H∞ Optimal Controller Design for The Small Unmanned Aerial Vehicle

Published Online: Feb 01, 2019

Page range: 313 - 322

DOI: https://doi.org/10.2478/raft-2018-0039

Keywords
UAV, modelling, automatic flight control system, dynamic optimal control, ∞ design

© 2018 Róbert Szabolcsi, published by Sciendo

This work is licensed under the Creative Commons Attribution-NonCommercial-NoDerivatives 4.0 License.

Robust H∞ Optimal Controller Design for The Small Unmanned Aerial Vehicle

Published Online: Feb 01, 2019

Page range: 313 - 322

DOI: https://doi.org/10.2478/raft-2018-0039

KeywordsUAV, modelling, automatic flight control system, dynamic optimal control, ∞ design

© 2018 Róbert Szabolcsi, published by Sciendo

This work is licensed under the Creative Commons Attribution-NonCommercial-NoDerivatives 4.0 License.

Keywords
UAV, modelling, automatic flight control system, dynamic optimal control, ∞ design