Robust Structural Design of an Active Aeroelastic Wing with Maneuver Load Inaccuracies
Author:
Affiliation:
1. Georgia Institute of Technology, Atlanta, Georgia 30332-0150
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.64
Reference21 articles.
1. Active Aeroelastic Wing Flight Research Program: Technical Program and Model Analytical Development
2. An active flexible wing multi-disciplinary design optimization method
3. Integration of a generic flight control system into ASTROS
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