Modeling and control of UAV quadrotor

Simple item page
dc.contributor.authorZammoum Boushaki, Razika
dc.contributor.authorAribi, Yacine
dc.contributor.authorLoubar, Hocine
dc.contributor.authorHamza, Younes
dc.contributor.authorKouzou, Abdellah
dc.date.accessioned2021-03-23T07:52:43Z
dc.date.available2021-03-23T07:52:43Z
dc.date.issued2019
dc.description.abstractSince the advances in technologies and the ability to manufacture miniature sensors and controllers using the Micro-Electro-Mechanical Systems (MEMS) technologies, there have been a lot of advances in the Unmanned Aerial Vehicle (UAV) area. A lot of the research conducted focused on the quadrotor due to its previously mentioned advantages of easier manufacturing, compactness and maneuverability among others. a detailed description of the dynamic modelling of the Quadrotor is presented. Various control strategies like the Proportional Derivative Control, the Sliding Mode Control and the Backstepping Control methods have been elucidated and implemented in MATLAB and SIMULINK. Simulations have been carried out and the results have been presenteden_US
dc.identifier.isbn978-172812726-2
dc.identifier.uriDOI: 10.1109/ICPEA1.2019.8911195
dc.identifier.urihttps://ieeexplore.ieee.org/document/7086762
dc.identifier.urihttps://dspace.univ-boumerdes.dz/handle/123456789/6668
dc.language.isoenen_US
dc.publisherIEEEen_US
dc.relation.ispartofseries2019 4th International Conference on Power Electronics and their Applications (ICPEA)
dc.subjectBackstepping controlen_US
dc.subjectModelingen_US
dc.subjectQuadrotoren_US
dc.subjectSliding Mode Controlen_US
dc.titleModeling and control of UAV quadrotoren_US
dc.typeOtheren_US

Files

License bundle

Now showing 1 - 1 of 1
No Thumbnail Available
Name:
license.txt
Size:
1.71 KB
Format:
Item-specific license agreed upon to submission
Description:
Download

Collections

Communications Internationales