Order Reduction of State-Space Aeroelastic Models Using Optimal Modal Analysis
Author:
Affiliation:
1. Boeing Commercial Aircraft, Seattle, Washington 98124-2207
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.14430
Reference14 articles.
1. Design for Active Flutter Suppression and Gust Alleviation Using State-Space Aeroelastic Modeling
2. Multiple order pole pure lag rational function approximations for unsteady aerodynamics
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