Efficient Framework for Missile Design and 6DoF Simulation using Multi-fidelity Analysis and Data Fusion
Author:
Affiliation:
1. Konkuk University
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2016-3365
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1. Digital virtual flight testing and evaluation method for flight characteristics airworthiness compliance of civil aircraft based on HQRM
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