GPS signal enhancement and attitude determination for a mini and low-cost unmanned aerial vehicle

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
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

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