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A Novel Control Allocation Method for Yaw Control of Tailless Aircraft (2020)

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/10.3390/aerospace7100150

Publication URI: http://dx.doi.org/10.3390/aerospace7100150

Type: Journal Article/Review

Parent Publication: Aerospace

Issue: 10