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

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 labo...

Full description

Bibliographic Details
Main Authors: Ahmad, S.M (Author), Shaheed, M.H (Author), Chipperfield, A.J (Author), Tokhi, M.O (Author)
Format: Article
Language:English
Published: 2002.
Subjects:
Online Access:Get fulltext