This paper presents results of a flight test of the L-1 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 for piloted tasks performed during the flight test.
Flight Test of an L(sub 1) Adaptive Controller on the NASA AirSTAR Flight Test Vehicle
AIAA Guidance, Navigation and Control Conference ; 2010 ; Toronto, Canada
2010-08-02
Aufsatz (Konferenz)
Keine Angabe
Englisch
L~1 Adaptive Control Design for NASA AirSTAR Flight Test Vehicle
British Library Conference Proceedings | 2009
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