Control of a Wing Section Using Leading-and Trailing-edge Flaps By L1 Adaptive Feedback Despite Disturbances

Authors

K. W. Lee, University of KwandongFollow
Sahjendra N. Singh, University of Nevada, Las VegasFollow

Document Type

Conference Proceeding

Publication Date

1-7-2013

Publication Title

51st AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition 2013, January 7, 2013 - January 10, 2013

Publisher

(ARC) Aerospace Research Central

Language

English

Repository Citation

Lee, K. W., Singh, S. N. (2013). Control of a Wing Section Using Leading-and Trailing-edge Flaps By L1 Adaptive Feedback Despite Disturbances. 51st AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition 2013, January 7, 2013 - January 10, 2013 (ARC) Aerospace Research Central.