GLA and Flutter Suppression for a SensorCraft Class Concept Using System Identification
Author:
Affiliation:
1. Lockheed Martin Aeronautics Company
2. Air Force Research Lab / RBAA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2008-7188
Reference10 articles.
1. 2Zink, S., Love, M., and Youngren, H. "Drag Minimization Through the use of Mission Adaptive Trailing Edge Flaps and Fuel StateControl", AIAA-2004-4365
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3. Reliability Analysis for an Unmanned Aerial Vehicle
4. Design and Analysis of HiLDA/AEI Aeroelastic Wind Tunnel Model
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