This paper presents results of a flight test of the L1 adaptive control architecture designed to directly compensate for significant uncertain cross-coupling in nonlinear systems. The flight test was conducted on the subscale turbine powered Generic Transport Model that is an integral part of the Airborne Subscale Transport Aircraft Research system at the NASA Langley Research Center. The results presented are in support of nonlinear aerodynamic modeling and instrumentation calibration.
LaPlace Transform1 Adaptive Control Law in Support of Large Flight Envelope Modeling Work
2011
12 pages
Report
No indication
English
Flight Test of L~1 Adaptive Control Law: Offset Landings and Large Flight Envelope Modeling Work
British Library Conference Proceedings | 2011
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