Conference papers
A two level non linear inverse control structure for rotorcraft trajectory tracking
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 [6 references]
https://hal-enac.archives-ouvertes.fr/hal-00938173
Contributor : Laurence Porte <>
Submitted on : Monday, June 23, 2014 - 4:01:08 PM
Last modification on : Friday, July 10, 2020 - 1:01:32 PM
Document(s) archivé(s) le : Tuesday, September 23, 2014 - 10:41:56 AM
Contributor : Laurence Porte <>
Submitted on : Monday, June 23, 2014 - 4:01:08 PM
Last modification on : Friday, July 10, 2020 - 1:01:32 PM
Document(s) archivé(s) le : Tuesday, September 23, 2014 - 10:41:56 AM
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