Conference papers
Rotorcraft trajectory tracking by non linear inverse control
Abstract : The purpose of this communication is to investigate the usefulness of the non linear inverse 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 inverse approach is then proposed. A supervision level is introduced to take into account the actuator limitations.
Cited literature [7 references]
https://hal-enac.archives-ouvertes.fr/hal-00938738
Contributor : Laurence Porte <>
Submitted on : Tuesday, April 29, 2014 - 3:02:10 PM
Last modification on : Tuesday, February 11, 2020 - 1:59:58 PM
Document(s) archivé(s) le : Tuesday, July 29, 2014 - 10:46:23 AM
Contributor : Laurence Porte <>
Submitted on : Tuesday, April 29, 2014 - 3:02:10 PM
Last modification on : Tuesday, February 11, 2020 - 1:59:58 PM
Document(s) archivé(s) le : Tuesday, July 29, 2014 - 10:46:23 AM
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