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Aeroservoelastic Modeling of Body Freedom Flutter for Control System DesignThe communication of this method is being used by NASA in the ongoing collaborations with groups interested in the X-56A flight test program. Model generation for body freedom flutter Addressing issues in: State Consistency, Low frequency dynamics, Unsteady aerodynamics. Applied approach to X-56A MUTT: Comparing to flight test data.
Document ID
20170003026
Acquisition Source
Armstrong Flight Research Center
Document Type
Presentation
Authors
Ouellette, Jeffrey (NASA Armstrong Flight Research Center Edwards, CA United States)
Date Acquired
April 6, 2017
Publication Date
March 29, 2017
Subject Category
Aircraft Stability And Control
Aerodynamics
Report/Patent Number
AFRC-E-DAA-TN40222
Meeting Information
Meeting: Aerospace Control and Guidance Systems Committee Meeting No. 119
Location: Fairborn, OH
Country: United States
Start Date: March 29, 2017
End Date: March 31, 2017
Sponsors: Society of Automotive Engineers, Inc., Institute of Electrical and Electronics Engineers
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
Degree of Freedom
Control systems

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