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IRAC Full-Scale Flight Testbed Capabilities (2009)

Hanson, Curtis E. ; Bosworth, John T. ; Cogan, Bruce R. ; [et al.]

In: CASI

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Publication Date: 2019-07-13

Description: 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.

Keywords: Aircraft Design, Testing and Performance

Type: DFRC-1044 , NASA IRAC RFI Response Workshop; Aug 09, 2009; Chicago, IL; United States

Format: application/pdf

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