In this paper we present a new L(sub 1) adaptive control architecture that directly compensates for matched as well as unmatched system uncertainty. To evaluate the L(sub 1) adaptive controller, we take advantage of the flexible research environment with rapid prototyping and testing of control laws in the Airborne Subscale Transport Aircraft Research system at the NASA Langley Research Center. We apply the L(sub 1) adaptive control laws to the subscale turbine powered Generic Transport Model. The presented results are from a full nonlinear simulation of the Generic Transport Model and some preliminary pilot evaluations of the L(sub 1) adaptive control law.
L(sub 1) Adaptive Control Design for NASA AirSTAR Flight Test Vehicle
AIAA Guidance, Navigation, and Control Conference (GNC) 2009 ; 2009 ; Chicago, IL, United States
2009-08-10
Sonstige
Keine Angabe
Englisch
L~1 Adaptive Control Design for NASA AirSTAR Flight Test Vehicle
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