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On the Take-Off of a Single-Wing Quadrotor

Abstract : This paper focusses on differential thrust quadcopters, whose flight envelope can be divided in two, namely: the quadrotor flight envelope, and the airplane flight envelope. We define a transition maneuver as a controlled path followed by an aircraft in order to move between the two flight envelopes. We propose a control law that is robust with respect to wind disturbances and unmodeled aerodynamic effects. This approach ensures that the aircraft does not fall down during the transition maneuver.
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Contributor : Michel MALABRE Connect in order to contact the contributor
Submitted on : Friday, March 19, 2021 - 2:43:34 PM
Last modification on : Monday, June 27, 2022 - 3:03:20 AM


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  • HAL Id : hal-03174745, version 1


N A Aguillón, M Bonilla, S Salazar, Michel Malabre, V Azhmyakov. On the Take-Off of a Single-Wing Quadrotor. European Control Conference ECC21, Jun 2021, Rotterdam, Netherlands. ⟨hal-03174745⟩



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