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Optimal Control Allocation with Load Sensor Feedback for Active Load SuppressionThese slide sets describe the OCLA formulation and associated algorithms as a set of new technologies in the first practical application of load limiting flight control utilizing load feedback as a primary control measurement. Slide set one describes Experiment Development and slide set two describes Flight-Test Performance.
Document ID
20170000506
Acquisition Source
Armstrong Flight Research Center
Document Type
Presentation
Authors
Miller, Christopher (NASA Armstrong Flight Research Center Edwards, CA, United States)
Date Acquired
January 19, 2017
Publication Date
January 9, 2017
Subject Category
Aircraft Stability And Control
Air Transportation And Safety
Report/Patent Number
DFRC-E-DAA-TN38390-1
Meeting Information
Meeting: AIAA SciTech 2017
Location: Grapevine, TX
Country: United States
Start Date: January 9, 2017
End Date: January 13, 2017
Sponsors: American Inst. of Aeronautics and Astronautics
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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