Please use this identifier to cite or link to this item:
|Title:||Construction, modeling and control of a mini autonomous UAV helicopter||Authors:||Cai, G.
First principle modeling
Flight control law
Onboard computer system
|Issue Date:||2008||Citation:||Cai, G.,Cai, A.K.,Chen, B.M.,Lee, T.H. (2008). Construction, modeling and control of a mini autonomous UAV helicopter. Proceedings of the IEEE International Conference on Automation and Logistics, ICAL 2008 : 449-454. ScholarBank@NUS Repository. https://doi.org/10.1109/ICAL.2008.4636193||Abstract:||We present in the paper the comprehensive design procedure of a mini UAV helicopter, called BabyLion. The hardware construction, along with the selection of all of necessary components, will be introduced. Since the system identification method is only partially suitable for the self-built BabyLion, we propose a more suitable parameter identification approach which combines both system identification and first principle modeling techniques to obtain a high fidelity linear model for hover and near hover flight conditions. A flight control law, which is based on the linear quadratic Gaussian (LQG) method and dynamic inversion approach, has been designed for the realization of automatic control. Simulation result and practical implementation results have proved that the designed controller is suitable. © 2008 IEEE.||Source Title:||Proceedings of the IEEE International Conference on Automation and Logistics, ICAL 2008||URI:||http://scholarbank.nus.edu.sg/handle/10635/69710||ISBN:||9781424425020||DOI:||10.1109/ICAL.2008.4636193|
|Appears in Collections:||Staff Publications|
Show full item record
Files in This Item:
There are no files associated with this item.
checked on Sep 18, 2019
checked on Sep 8, 2019
Items in DSpace are protected by copyright, with all rights reserved, unless otherwise indicated.