Adaptive Variable Structure Control of Aircraft with an Unknown High-Frequency Gain Matrix
Author:
Affiliation:
1. University of Kwandong, Kangwon 210-701, South Korea
2. University of Nevada, Las Vegas, Las Vegas, Nevada 89154-4026
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Applied Mathematics,Electrical and Electronic Engineering,Space and Planetary Science,Aerospace Engineering,Control and Systems Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.31209
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