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IRAC Full-Scale Flight Testbed CapabilitiesOverview: Provide validation of adaptive control law concepts through full scale flight evaluation in a representative avionics architecture. Develop an understanding of aircraft dynamics of current vehicles in damaged and upset conditions Real-world conditions include: a) Turbulence, sensor noise, feedback biases; and b) Coupling between pilot and adaptive system. Simulated damage includes 1) "B" matrix (surface) failures; and 2) "A" matrix failures. Evaluate robustness of control systems to anticipated and unanticipated failures.
Document ID
20090033937
Acquisition Source
Armstrong Flight Research Center
Document Type
Presentation
Authors
Lee, James A. (NASA Dryden Flight Research Center Edwards, CA, United States)
Pahle, Joseph (NASA Dryden Flight Research Center Edwards, CA, United States)
Cogan, Bruce R. (NASA Dryden Flight Research Center Edwards, CA, United States)
Hanson, Curtis E. (NASA Dryden Flight Research Center Edwards, CA, United States)
Bosworth, John T. (NASA Dryden Flight Research Center Edwards, CA, United States)
Date Acquired
August 24, 2013
Publication Date
August 9, 2009
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
DFRC-1044
Report Number: DFRC-1044
Meeting Information
Meeting: NASA IRAC RFI Response Workshop
Location: Chicago, IL
Country: United States
Start Date: August 9, 2009
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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