Integration of Multi-Fidelity Methods for Generating an Aerodynamic Model for Flight Simulation
Author:
Affiliation:
1. University of Liverpool
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2008-197
Reference22 articles.
1. Evolution of flight vehicle system identification
2. High-Order Polynomial Response Surface with Optimal Selection of Interaction Terms
3. Computational Methods for Stability and Control (COMSAC): The Time Has Come
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