Nonlinear Control of a Prototypical Wing Section with Torsional Nonlinearity
Author:
Affiliation:
1. Texas A&M University, College Station, Texas 77843-3141
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/10.2514/2.4174
Reference29 articles.
1. 1Fung, Y. C., An Introduction to the Theory of Aeroelasticity, Wiley, New York, 1955, pp.207-215.
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