Spin Aerodynamic Modeling for a Fixed-Wing Aircraft Using Flight Data
Author:
Affiliation:
1. Virginia Polytechnic Institute and State University
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2022-1160
Reference35 articles.
1. Multiple input design for real-time parameter estimation in the frequency domain
2. Global Hawk Systems Engineering. Case Study
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