A geometric controller based on dynamic feedback linearization achieves almost-global asymptotic stability for attitude tracking on a novel underactuated swiveling biplane-quadrotor tailsitter.
Design, performance and test- ing of a quad rotor biplane micro air vehicle for multi role missions
1 Pith paper cite this work. Polarity classification is still indexing.
1
Pith paper citing it
fields
eess.SY 1years
2019 1verdicts
UNVERDICTED 1representative citing papers
citing papers explorer
-
Attitude Control of a Novel Tailsitter: Swiveling Biplane-Quadrotor
A geometric controller based on dynamic feedback linearization achieves almost-global asymptotic stability for attitude tracking on a novel underactuated swiveling biplane-quadrotor tailsitter.