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Flight Test of Composite Model Reference Adaptive Control (CMRAC) Augmentation Using NASA AirSTAR InfrastructureThis paper presents flight test results of a robust linear baseline controller with and without composite adaptive control augmentation. The flight testing was conducted using the NASA Generic Transport Model as part of the Airborne Subscale Transport Aircraft Research system at NASA Langley Research Center.
Document ID
20110014624
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Gregory, Irene M.
(NASA Langley Research Center Hampton, VA, United States)
Gadient, ROss
(Boeing Co. Huntington Beach, CA, United States)
Lavretsky, Eugene
(Boeing Co. Huntington Beach, CA, United States)
Date Acquired
August 25, 2013
Publication Date
August 8, 2011
Subject Category
Aircraft Stability And Control
Report/Patent Number
NF1676L-12010
Report Number: NF1676L-12010
Meeting Information
Meeting: AIAA Guidance, Navigation, and Control Conference
Location: Portland, OR
Country: United States
Start Date: August 8, 2011
End Date: August 11, 2011
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
WBS: WBS 457280.02.07.07.02.01
CONTRACT_GRANT: NNL06AA04B
Distribution Limits
Public
Copyright
Public Use Permitted.
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