UCAV model design and static experimental investigations to estimate control device effectiveness and S&C capabilities
Author:
Affiliation:
1. German Aerospace Center (DLR)
2. NASA Langley Research Center
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2014-2002
Reference18 articles.
1. Low-speed Dynamic Wind Tunnel Test Analysis of a Generic 53° Swept UCAV Configuration
2. Integrated Computational/Experimental Approach to Unmanned Combat Air Vehicle Stability and Control Estimation
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