Non-linear modelling of a one-degree-of-freedom twin-rotor multi-input multi-output system using radial basis function networks

Author:

Ahmad S M1,Shaheed M H2,Chipperfield A J3,Tokhi M O3

Affiliation:

1. The University of Plymouth Department of Mechanical and Marine Engineering UK

2. Queen Mary University of London Department of Engineering UK

3. The University of Sheffield Department of Automatic Control and Systems Engineering UK

Abstract

Modelling of innovative aircraft such as unmanned air vehicles (UAVs), X-wing, tilt body and delta-wing aircraft is not easy. It is argued in this paper that non-linear system identification is suitable for modelling air vehicles of complex configuration. This approach is demonstrated through a laboratory test rig. Extensive time and frequency-domain model-validation tests are employed in order to instil confidence in the estimated model. The estimated model has a good predictive capability and can be utilized for non-linear flight simulation studies. Some aspects of the modelling approach presented may be relevant to flight mechanics modelling of new generations of air vehicle.

Publisher

SAGE Publications

Subject

Mechanical Engineering,Aerospace Engineering

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