Fuzzy Logic Method Use in F/A-18 Aircraft Model Identification
Author:
Affiliation:
1. École de Technologie Supérieure, Montréal, Quebec H3C 1K3, Canada
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.40714
Reference19 articles.
1. Static Aeroelastic and Open-Loop Aeroservoelastic Analyses for the F/A-18 AAW Aircraft
2. The X-53 A Summary of the Active Aeroelastic Wing Flight Research Program
3. Nonlinear Aeroelastic System Identification with Application to Experimental Data
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