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|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|
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