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Mathematical Problems in Engineering
Volume 2015, Article ID 938246, 7 pages
http://dx.doi.org/10.1155/2015/938246
Research Article

Integral Sliding Mode Control for Helicopter via Disturbance Observer and Quantum Information Technique

1College of Automation Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China
2Department of Electrical and Computer Engineering, University of Virginia, Charlottesville, VA 22903, USA

Received 6 August 2014; Accepted 19 September 2014

Academic Editor: Ke Zhang

Copyright © 2015 Qiang Qu et al. This is an open access article distributed under the Creative Commons Attribution License, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.

How to Cite this Article

Qiang Qu, Fuyang Chen, Bin Jiang, and Gang Tao, “Integral Sliding Mode Control for Helicopter via Disturbance Observer and Quantum Information Technique,” Mathematical Problems in Engineering, vol. 2015, Article ID 938246, 7 pages, 2015. https://doi.org/10.1155/2015/938246.