Conference papers
Differential flat control for rotorcraft trajectory tracking
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.
Cited literature [10 references]
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, February 11, 2020 - 1:59:57 PM
Document(s) archivé(s) le : Tuesday, July 29, 2014 - 10:45:56 AM
Contributor : Laurence Porte <>
Submitted on : Tuesday, April 29, 2014 - 3:17:58 PM
Last modification on : Tuesday, February 11, 2020 - 1:59:57 PM
Document(s) archivé(s) le : Tuesday, July 29, 2014 - 10:45:56 AM
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