Please use this identifier to cite or link to this item: https://doi.org/10.1177/0142331209342220
Title: GPS signal enhancement and attitude determination for a mini and low-cost unmanned aerial vehicle
Authors: Yun, B.
Cai, G. 
Chen, B.M. 
Peng, K. 
Lum, K.Y. 
Keywords: attitude reference systems
H∞ filtering
unmanned aerial vehicles
Issue Date: Aug-2011
Source: 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
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