Differential flat control for rotorcraft trajectory trackingReport as inadecuate

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1 ENAC - Ecole Nationale de l-Aviation Civile 2 LAAS-DISCO - Équipe DIagnostic, Supervision et COnduite LAAS - Laboratoire d-analyse et d-architecture des systèmes Toulouse

Abstract : The purpose of this communication is to investigate the usefulness of the differential flatness control approach to solve the trajectory tracking problem for a four rotor aircraft. After introducing simplifying assumptions, the flight dynamics equations for the four rotor aircraft are considered. A trajectory tracking control structure based on a two layer non linear approach is then proposed. A supervision level is introduced to take into account the actuators limitations.

Keywords : differential flatness guidance supervision rotorcraft flight mechanics trajectory tracking

Author: Nan Zhang - Geanina Andrei - Antoine Drouin - Felix Antonio Claudio Mora-Camino -

Source: https://hal.archives-ouvertes.fr/


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