These slides describe a method and technology of modeling flexible aircraft for active control of structural dynamics. Objective: Generate models useful for the design and evaluation of control laws for active structural control and flutter suppression that are able to accurately predict body freedom flutter.
Lessons from Modeling Flexible Aircraft for Active Flutter Suppression
2019
27 pages
Report
Keine Angabe
Englisch
Active flutter suppression on an F-4F aircraft
AIAA | 1980
|Active Flutter Suppression on an F-4F Aircraft
AIAA | 1982
|Wiley | 2016
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