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.
IRAC Full-Scale Flight Testbed Capabilities
2009
17 pages
Report
No indication
English
IRAC Full-Scale Flight Testbed Capabilities
NTRS | 2009
|NTRS | 2008
|NTIS | 2008
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