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
Aerospace Control and Guidance Systems Committee (ACGSC) Meeting ; 2019 ; Santa Fe, NM, United States
2019-03-27
Miscellaneous
No indication
English
Active Flutter Suppression on an F-4F Aircraft
AIAA | 1982
|Active flutter suppression on an F-4F aircraft
AIAA | 1980
|Wiley | 2016
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