Backstepping Control of Drone †

dc.contributor.authorSaibi, Ali
dc.contributor.authorBoushaki, Razika
dc.contributor.authorBelaidi, Hadjira
dc.date.accessioned2023-07-12T09:41:56Z
dc.date.available2023-07-12T09:41:56Z
dc.date.issued2022
dc.description.abstractThis work derives the models which can be used to design and implement control laws for six degrees-of-freedom (DOF) quadrotor stability. The first part of this paper deals with the presentation of the background of quadrotor modeling; the second part describes the direct control of the drone using the backstepping control principal. This principal is based on the division of the system into several sub-systems in a cascade, which makes the control laws generated on each subsystem, in a decreasing manner, until a global control law for the whole system is generated. The simulation results for the sm controller are generated on the MATLAB/Simulink platform; the results show a good performance in both the transient and steady-state operations.en_US
dc.identifier.issn2673-4591
dc.identifier.urihttps://doi.org/10.3390/ engproc2022014004
dc.identifier.urihttps://dspace.univ-boumerdes.dz/handle/123456789/11932
dc.language.isoenen_US
dc.publisherMDPIen_US
dc.relation.ispartofseriesEngineering Proceedings/Vol. 14, N° 4;
dc.subjectQuadrotoren_US
dc.subjectDynamic modelen_US
dc.subjectBacksteppingen_US
dc.titleBackstepping Control of Drone †en_US
dc.typeArticleen_US

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