Neural network based feedback error controller for helicopter

Neural network based feedback error controller for helicopter Purpose – This paper seeks to present a feedback error learning neuro‐controller for an unstable research helicopter. Design/methodology/approach – Three neural‐aided flight controllers are designed to satisfy the ADS‐33 handling qualities specifications in pitch, roll and yaw axes. The proposed controller scheme is based on feedback error learning strategy in which the outer loop neural controller enhances the inner loop conventional controller by compensating for unknown non‐linearity and parameter uncertainties. The basic building block of the neuro‐controller is a nonlinear auto regressive exogenous (NARX) input neural network. For each neural controller, the parameter update rule is derived using Lyapunov‐like synthesis. An offline finite time training is used to provide asymptotic stability and on‐line learning strategy is employed to handle parameter uncertainty and nonlinearity. Findings – The theoretical results are validated using simulation studies based on a nonlinear six degree‐of‐freedom helicopter undergoing an agile maneuver. The neural controller performs well in disturbance rejection is the presence of gust and sensor noise. Practical implications – The neuro‐control approach presented in this paper is well suited to unmanned and small‐scale helicopters. Originality/value – The study shows that the neuro‐controller meets the requirements of ADS‐33 handling qualities specifications of a helicopter. http://www.deepdyve.com/assets/images/DeepDyve-Logo-lg.png Aircraft Engineering and Aerospace Technology Emerald Publishing

Neural network based feedback error controller for helicopter

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Publisher
Emerald Publishing
Copyright
Copyright © 2011 Emerald Group Publishing Limited. All rights reserved.
ISSN
0002-2667
DOI
10.1108/00022661111159898
Publisher site
See Article on Publisher Site

Abstract

Purpose – This paper seeks to present a feedback error learning neuro‐controller for an unstable research helicopter. Design/methodology/approach – Three neural‐aided flight controllers are designed to satisfy the ADS‐33 handling qualities specifications in pitch, roll and yaw axes. The proposed controller scheme is based on feedback error learning strategy in which the outer loop neural controller enhances the inner loop conventional controller by compensating for unknown non‐linearity and parameter uncertainties. The basic building block of the neuro‐controller is a nonlinear auto regressive exogenous (NARX) input neural network. For each neural controller, the parameter update rule is derived using Lyapunov‐like synthesis. An offline finite time training is used to provide asymptotic stability and on‐line learning strategy is employed to handle parameter uncertainty and nonlinearity. Findings – The theoretical results are validated using simulation studies based on a nonlinear six degree‐of‐freedom helicopter undergoing an agile maneuver. The neural controller performs well in disturbance rejection is the presence of gust and sensor noise. Practical implications – The neuro‐control approach presented in this paper is well suited to unmanned and small‐scale helicopters. Originality/value – The study shows that the neuro‐controller meets the requirements of ADS‐33 handling qualities specifications of a helicopter.

Journal

Aircraft Engineering and Aerospace TechnologyEmerald Publishing

Published: Sep 6, 2011

Keywords: Neural network; Helicopters; Control; Handling qualities

References

  • Probabilistic robust control of rotorcraft
    Horn, J.F.; Tolani, D.K.; Lagoa, C.M.; Wang, Q.; Ray, A.
  • Design of a stability augmentation system for a helicopter using LQR control and ADS‐33 handling qualities specifications
    Vijaya Kumar, M.; Suresh, S.; Omkar, S.N.; Ganguli, R.; Sampath, P.
  • Multivariable control of the longitudinal and lateral dynamics of a fly‐by‐wire helicopter
    Walker, D.J.

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