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Beyond Rigid Body: Integrated Structural Control of Extremely Lightweight Flexible AircraftTop level description of work on integrated structural control of extremely lightweight flexible aircraft. Includes motivation and challenges as well as a description of the X-56A vehicle.
Document ID
20120015944
Acquisition Source
Armstrong Flight Research Center
Document Type
Presentation
Authors
Bosworth, John T. (NASA Dryden Flight Research Center Edwards, CA, United States)
Date Acquired
August 26, 2013
Publication Date
June 1, 2012
Subject Category
Aircraft Stability And Control
Report/Patent Number
DFRC-E-DAA-TN5285
Report Number: DFRC-E-DAA-TN5285
Meeting Information
Meeting: NESC Guidance and Controls Face-to-Face Meeting
Location: Hampton, VA
Country: United States
Start Date: June 12, 2012
Funding Number(s)
WBS: WBS 561581.02.08.02.43.05.06
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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