IEEE - Institute of Electrical and Electronics Engineers, Inc. - Variable structure control law design for helicopter based on output feedback

2009 4th IEEE Conference on Industrial Electronics and Applications (ICIEA)

Author(s): Lu, J.C. ; Zhang, J.M.
Publisher: IEEE - Institute of Electrical and Electronics Engineers, Inc.
Publication Date: 1 May 2009
Conference Location: Xian, China, China
Conference Date: 25 May 2009
Page(s): 1,621 - 1,624
ISBN (CD): 978-1-4244-2800-7
ISBN (Paper): 978-1-4244-2799-4
DOI: 10.1109/ICIEA.2009.5138469
Regular:

In this paper, a sliding mode control law for helicopter is presented. The control law is based on the newly developed sliding mode control theory which is called sliding mode output feedback... View More

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