Please use this identifier to cite or link to this item:
|Title:||GPS signal enhancement and attitude determination for a mini and low-cost unmanned aerial vehicle||Authors:||Yun, B.
|Keywords:||attitude reference systems
unmanned aerial vehicles
|Issue Date:||Aug-2011||Citation:||Yun, B., Cai, G., Chen, B.M., Peng, K., Lum, K.Y. (2011-08). GPS signal enhancement and attitude determination for a mini and low-cost unmanned aerial vehicle. Transactions of the Institute of Measurement and Control 33 (6) : 665-682. ScholarBank@NUS Repository. https://doi.org/10.1177/0142331209342220||Abstract:||We present in this paper an integration scheme of a low-cost inertial attitude and position reference system for a mini unmanned helicopter by utilizing the robust and H∞ filtering technique. The result has been successfully implemented and tested on our mini-scale unmanned helicopter. Simulation and flight experiment results show that the proposed technique is very effective in real-time and suitable for control, stabilization and navigation for mini-scale unmanned air vehicles. © 2010 The Institute of Measurement and Control.||Source Title:||Transactions of the Institute of Measurement and Control||URI:||http://scholarbank.nus.edu.sg/handle/10635/82423||ISSN:||01423312||DOI:||10.1177/0142331209342220|
|Appears in Collections:||Staff Publications|
Show full item record
Files in This Item:
There are no files associated with this item.
checked on Nov 21, 2022
WEB OF SCIENCETM
checked on Nov 11, 2022
checked on Nov 24, 2022
Items in DSpace are protected by copyright, with all rights reserved, unless otherwise indicated.