Please use this identifier to cite or link to this item:
|Title:||Nonlinear modeling of a miniature fixed-pitch coaxial UAV||Authors:||Wang, F.
micro unmanned aerial vehicle
|Issue Date:||2012||Citation:||Wang, F.,Phang, S.K.,Cui, J.,Cai, G.,Chen, B.M.,Lee, T.H. (2012). Nonlinear modeling of a miniature fixed-pitch coaxial UAV. Proceedings of the American Control Conference : 3863-3870. ScholarBank@NUS Repository.||Abstract:||This paper presents the work that has been done to derive an accurate nonlinear model for a miniature fixed-pitch coaxial helicopter. Starting from the Newton-Euler rigid body dynamic equations, forces and torques generated at various parts of the UAV have been identified and formulated. The physical meanings behind the model are clearly explained, and the methods of identifying all the important model parameters are also provided. The full model is verified by comparing simulation results and actual flight tests with the NUS FeiLion coaxial UAV. The agreement between the two is promising. © 2012 AACC American Automatic Control Council).||Source Title:||Proceedings of the American Control Conference||URI:||http://scholarbank.nus.edu.sg/handle/10635/51222||ISBN:||9781457710957||ISSN:||07431619|
|Appears in Collections:||Staff Publications|
Show full item record
Files in This Item:
There are no files associated with this item.
checked on Jan 13, 2022
Items in DSpace are protected by copyright, with all rights reserved, unless otherwise indicated.