IEEE - Institute of Electrical and Electronics Engineers, Inc. - Attitude Control System Design for Unmanned Aerial Vehicles using H-Infinity and Loop-shaping Methods

2007 IEEE International Conference on Control and Automation, ICCA 2007

Author(s): J. Gadewadikar ; F. Lewis ; K. Subbarao ; B.M. Chen
Publisher: IEEE - Institute of Electrical and Electronics Engineers, Inc.
Publication Date: 1 May 2007
Conference Location: Guangzhou, China
Conference Date: 30 May 2007
Page(s): 1,174 - 1,179
ISBN (CD): 978-1-4244-0818-4
ISBN (Paper): 978-1-4244-0817-7
DOI: 10.1109/ICCA.2007.4376545
Regular:

The aim of this paper is to design a helicopter attitude control system with guaranteed performance that allows tracking control of all three attitudes-roll, pitch, and yaw, while preserving a... View More

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