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A Control Allocation Method to Reduce Roll-Yaw coupling on Tailless Aircraft (2021)

First Author: Shearwood T

Attributed to: Control of spanwise flow induced separation on swept low aspect ratio wings to improve controllability funded by EPSRC

Abstract

No abstract provided

Bibliographic Information

Digital Object Identifier: http://dx.doi.org/10.2514/6.2021-1826

Publication URI: http://dx.doi.org/10.2514/6.2021-1826

Type: Conference/Paper/Proceeding/Abstract