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Please use this identifier to cite or link to this item: http://dspace.bits-pilani.ac.in:8080/jspui/handle/123456789/9935
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dc.contributor.authorMukherjee, Bijoy Krishna-
dc.date.accessioned2023-03-24T05:41:19Z-
dc.date.available2023-03-24T05:41:19Z-
dc.date.issued2022-03-
dc.identifier.urihttps://www.emerald.com/insight/content/doi/10.1108/AEAT-08-2021-0231/full/html-
dc.identifier.urihttp://dspace.bits-pilani.ac.in:8080/xmlui/handle/123456789/9935-
dc.description.abstractUnmanned aerial vehicles (UAVs) have wide applications in surveillance and reconnaissance without risking human life. Due to unbalanced payload distribution or in-flight deployment, UAVs may undergo lateral center of gravity (c.g.) variations resulting in an asymmetric dynamic having significant longitudinal and lateral/directional coupling and hence more pronounced nonlinearity. Therefore, automatic control of UAVs becomes extremely difficult when it is forced to perform maneuvers under such imbalance in lateral mass distribution. The purpose of this paper is to design adaptive nonlinear control so that the UAV can perform some useful lateral/directional maneuver under lateral c.g. uncertainty.en_US
dc.language.isoenen_US
dc.publisherEmeralden_US
dc.subjectEEEen_US
dc.subjectUAVen_US
dc.subjectAdaptive controlen_US
dc.subjectBacksteppingen_US
dc.subjectCenter of gravityen_US
dc.subjectAileron rollen_US
dc.subjectHorizontal turn maneuveren_US
dc.titleAdaptive block backstepping control for a UAV performing lateral maneuvers under lateral c.g. uncertaintyen_US
dc.typeArticleen_US
Appears in Collections:Department of Electrical and Electronics Engineering

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