NASA NTRS · 20090033937
IRAC Full-Scale Flight Testbed Capabilities
Abstract
Overview: 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.
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Lee, James A., Pahle, Joseph, Cogan, Bruce R., Hanson, Curtis E., Bosworth, John T.. 2009-08-09. IRAC Full-Scale Flight Testbed Capabilities. https://ntrs.nasa.gov/citations/20090033937
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