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arXiv · 2311.02668

Control of convertible UAV with vectorized thrust

Tomas Lopes de Oliveira·Andre Anglade·Tarek Hamel·Claude Samson
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Abstract

This paper is an addition to an article previously published by three of the authors that addresses the control of convertible fixed-wing aircraft with vectorized thrust. The control solution here developed extends the one presented in the former paper by complementing it with a strategy for the hovering flight and a control policy to handle the transition phase between low and high airspeed. An estimator of the air velocity required in all flight phases is also proposed. Realistic simulation results on a tri-tilt rotor Unmanned Aerial Vehicle (UAV) illustrate and assess the methodology.

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Tomas Lopes de Oliveira, Andre Anglade, Tarek Hamel, Claude Samson. 2023-11-05. Control of convertible UAV with vectorized thrust. https://arxiv.org/abs/2311.02668

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