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Lessons from Modeling Flexible Aircraft for Active Flutter SuppressionThese 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.
Document ID
20190002087
Acquisition Source
Armstrong Flight Research Center
Document Type
Presentation
Authors
Ouellette, Jeffrey (NASA Armstrong Flight Research Center Edwards, CA, United States)
Date Acquired
April 1, 2019
Publication Date
March 27, 2019
Subject Category
Aircraft Stability And Control
Report/Patent Number
AFRC-E-DAA-TN66921
Meeting Information
Meeting: Aerospace Control and Guidance Systems Committee (ACGSC) Meeting
Location: Santa Fe, NM
Country: United States
Start Date: March 27, 2019
End Date: March 29, 2019
Sponsors: Institute of Electrical and Electronics Engineers
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
Lessons Learned

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