Please use this identifier to cite or link to this item: https://er.nau.edu.ua/handle/NAU/36934
Full metadata record
DC FieldValueLanguage
dc.contributor.authorKucherov, D.P.en
dc.contributor.authorKucherov, Dmytroen
dc.contributor.authorКучеров, Дмитро Павловичuk_UA
dc.contributor.authorКучеров, Дмитрий Павловичru
dc.date.accessioned2018-11-17T15:42:33Z-
dc.date.available2018-11-17T15:42:33Z-
dc.date.issued2018-11-16-
dc.identifier.issn2227-524X-
dc.identifier.urihttp://er.nau.edu.ua/handle/NAU/36934-
dc.descriptionSynthesis of the switching control law for a quadrotor autopiloten
dc.description.abstractThe paper deals with the problem of synthesizing the time-optimal control law by the angular coordinates of an unmanned aerial vehicle with stabilization in the pitch and roll directions. The full mathematical model of the unmanned aerial vehicle is reduced to a system of the first-order differential equations, based on which the optimal control law is constructed. Control action in each plane depends only on the measured coordinates and is calculated in real time. It is believed that the dynamic model, described by a system of differential equations, contains complex roots, which indicate the oscillatory response of the controlled object to the control action. Some properties of the switching line and switching control are also considered in the paper. Some results of simulating the dynamics of the object under examination with a synthesized control law are presented.en
dc.language.isoenen
dc.publisherSciencepubcoen
dc.subjectdynamic systemen
dc.subjectquadrotoren
dc.titleSynthesis of the switching control law for a quadrotor autopiloten
dc.typeArticleen
Appears in Collections:Наукові статті кафедри комп’ютеризованих систем управління

Files in This Item:
File Description SizeFormat 
IJET-2018.pdfОсновная статья492 kBAdobe PDFView/Open


Items in DSpace are protected by copyright, with all rights reserved, unless otherwise indicated.