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Maximilian Boosfeld

1 accepted papers

2016

Full Attitude Control of a VTOL tailsitter UAV

ICRA 2016

This paper addresses the challenges of the design, development and control of a new convertible VTOL tailsitter unmanned aerial vehicle that combines the advantages of both fixed wing and rotary wing systems. Wind tunnel measurements are used to get an understanding of the control allocation and to

Cited by 89SourceScholar