Performance of minimum energy controllers on tiltrotor aircraft

Performance of minimum energy controllers on tiltrotor aircraft Purpose – The purpose of this article is to evaluate performance of minimum energy controllers thoroughly on a tiltrotor aircraft. Approach – Minimum energy controllers are designed for tiltrotor aircraft models for helicopter and airplane modes. Performance of minimum energy controllers is evaluated with respect to several criteria. Findings – Minimum energy controllers can be used for tiltrotor aircraft flight control system design. These controllers show satisfactory performance when noise intensities and variance bounds vary. Practical implications – Minimum energy controllers can be implemented for tiltrotor aircraft flight control system design. Originality/value – In this paper, minimum energy controllers are applied for tiltrotor aircraft flight control system design and the performance of minimum energy controllers is evaluated deeply on a complex physical system (i.e. tiltrotor aircraft). http://www.deepdyve.com/assets/images/DeepDyve-Logo-lg.png Aircraft Engineering and Aerospace Technology: An International Journal Emerald Publishing

Performance of minimum energy controllers on tiltrotor aircraft

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Publisher
Emerald Publishing
Copyright
Copyright © Emerald Group Publishing Limited
ISSN
0002-2667
DOI
10.1108/AEAT-11-2012-0225
Publisher site
See Article on Publisher Site

Abstract

Purpose – The purpose of this article is to evaluate performance of minimum energy controllers thoroughly on a tiltrotor aircraft. Approach – Minimum energy controllers are designed for tiltrotor aircraft models for helicopter and airplane modes. Performance of minimum energy controllers is evaluated with respect to several criteria. Findings – Minimum energy controllers can be used for tiltrotor aircraft flight control system design. These controllers show satisfactory performance when noise intensities and variance bounds vary. Practical implications – Minimum energy controllers can be implemented for tiltrotor aircraft flight control system design. Originality/value – In this paper, minimum energy controllers are applied for tiltrotor aircraft flight control system design and the performance of minimum energy controllers is evaluated deeply on a complex physical system (i.e. tiltrotor aircraft).

Journal

Aircraft Engineering and Aerospace Technology: An International JournalEmerald Publishing

Published: Aug 26, 2014

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