<?xml version="1.0" encoding="UTF-8"?>
<records>
<record>
<language>eng</language>
<publisher>Science and Education Publishing</publisher>
<journalTitle>Journal of Automation and Control</journalTitle>
<eissn>2372-3041</eissn>
<publicationDate>2017-12-11</publicationDate>
<volume>5</volume>
<issue>2</issue>
<startPage>60</startPage>
<endPage>63</endPage>
<doi>10.12691/automation-5-2-6</doi>
<publisherRecordId>AUTOMATION2017526</publisherRecordId>
<documentType>article</documentType>
<title language="eng">Mathematical Modeling of Vertical Position Stability of Quadrocopter</title>
<authors>
<author>
<name>Michal Kelemen</name>
<affiliationId>1</affiliationId>
</author>
<author>
<name>Ivan Virgala</name>
<email>ivan.virgala@tuke.sk</email>
<affiliationId>1</affiliationId>
</author>
<author>
<name>Tomáš Lipták</name>
<affiliationId>1</affiliationId>
</author>
<author>
<name>Milan ?kurka</name>
<affiliationId>1</affiliationId>
</author>

</authors>
<affiliationsList>
<affiliationName affiliationId="1">Department of Mechatronics, Faculty of Mechanical Engineering, Technical University of Košice, Košice, Slovakia</affiliationName>



</affiliationsList>
<abstract language="eng">The paper deals with investigation of position stability of quadrocopter in vertical axis. At first, dynamic model of quadrocopter is introduced. In the paper are derived relations for control error in steady state for PD and PID controller. Based on dynamic model the PID controller is designed by optimizing method. Using designed controller the quadrocopter stability in vertical axis was simulated in software Matlab. The results of the simulation are discussed in the conclusion.</abstract>
<fullTextUrl format="pdf">http://pubs.sciepub.com/automation/5/2/6/automation-5-2-6.pdf</fullTextUrl>
<keywords language="eng"><keyword>dynamic model</keyword>
<keyword>modeling</keyword>
<keyword>quadrocopter</keyword>
<keyword>simulation</keyword>
</keywords>
</record>
</records>
