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Differential flat control for rotorcraft trajectory tracking

Nan Zhang 1 Geanina Andrei 1 Antoine Drouin 1 Felix Mora-Camino 2
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
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
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https://hal-enac.archives-ouvertes.fr/hal-00938210
Contributor : Laurence Porte <>
Submitted on : Tuesday, April 29, 2014 - 3:17:58 PM
Last modification on : Tuesday, October 20, 2020 - 10:32:06 AM
Long-term archiving on: : Tuesday, July 29, 2014 - 10:45:56 AM

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  • HAL Id : hal-00938210, version 1

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MAIAA-AUTO | ENAC | LAAS-DISCO | CNRS | LAAS | LAAS-DECISION-ET-OPTIMISATION | TDS-MACS | INSA-TOULOUSE | DRONES | INSA-GROUPE | UNIV-TLSE3 | OPTIM | UT1-CAPITOLE | UNIV-TLSE2

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Nan Zhang, Geanina Andrei, Antoine Drouin, Felix Mora-Camino. Differential flat control for rotorcraft trajectory tracking. IMECS 2009, International Multiconference of Engineers and Computer Scientists, Mar 2009, Hong Kong, China. pp 1331-1336. ⟨hal-00938210⟩

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