<?xml version="1.0" encoding="utf-8"?>
<journal>
<title>International Journal of Applied Operational Research</title>
<title_fa>ژورنال بین المللی پژوهش عملیاتی</title_fa>
<short_title>International Journal of Applied Operational Research - An Open Access Journal</short_title>
<subject>Basic Sciences</subject>
<web_url>http://ijorlu.lahijan.iau.ir</web_url>
<journal_hbi_system_id>1</journal_hbi_system_id>
<journal_hbi_system_user>admin</journal_hbi_system_user>
<journal_id_issn>2251-6867</journal_id_issn>
<journal_id_issn_online>2251-9432</journal_id_issn_online>
<journal_id_pii>8</journal_id_pii>
<journal_id_doi>7</journal_id_doi>
<journal_id_iranmedex></journal_id_iranmedex>
<journal_id_magiran></journal_id_magiran>
<journal_id_sid>14</journal_id_sid>
<journal_id_nlai>8888</journal_id_nlai>
<journal_id_science>13</journal_id_science>
<language>en</language>
<pubdate>
	<type>jalali</type>
	<year>1395</year>
	<month>10</month>
	<day>1</day>
</pubdate>
<pubdate>
	<type>gregorian</type>
	<year>2017</year>
	<month>1</month>
	<day>1</day>
</pubdate>
<volume>7</volume>
<number>1</number>
<publish_type>online</publish_type>
<publish_edition>1</publish_edition>
<article_type>fulltext</article_type>
<articleset>
	<article>


	<language>en</language>
	<article_id_doi></article_id_doi>
	<title_fa></title_fa>
	<title>Mathematical  Dynamics, Kinematics Modeling and PID Equation Controller Of  QuadCopter</title>
	<subject_fa>تخصصي</subject_fa>
	<subject>Special</subject>
	<content_type_fa>كاربردي</content_type_fa>
	<content_type>Applicable</content_type>
	<abstract_fa></abstract_fa>
	<abstract>&lt;strong&gt;Abstract &lt;/strong&gt;Quadcopter is the Unmanned Aerial Vehicle that can vertical tack off and landing. its useful platform for many applications in Commercial, civil or military . In this article ,we present&amp;nbsp; the Dynamics and Kinematics model of&amp;nbsp; quadcopter&amp;nbsp; and the effect of forces by introducing two frames on the ground and it&amp;rsquo;s body, also we design and implement the PID controller then found the best way of manual tuning for adjusting the PID&amp;nbsp; coefficient&amp;nbsp; in&amp;nbsp; Symmetric quadcopter , we use the 10 DOF IMU consist of&amp;nbsp; three axis gyroscope ,accelerometer and magnetometer with three PID&amp;nbsp; controller for Roll, Pitch, Yaw angle and the separate PID&amp;nbsp; controller for altitude of quadcopter Robot, also build it based on extracted result.&amp;nbsp;</abstract>
	<keyword_fa></keyword_fa>
	<keyword>Quad copter, PID controller, Dynamics model, Unmanned Aerial Vehicle</keyword>
	<start_page>77</start_page>
	<end_page>85</end_page>
	<web_url>http://ijorlu.lahijan.iau.ir/browse.php?a_code=A-10-403-1&amp;slc_lang=en&amp;sid=1</web_url>


<author_list>
	<author>
	<first_name>M.</first_name>
	<middle_name></middle_name>
	<last_name>Etemadi</last_name>
	<suffix></suffix>
	<first_name_fa></first_name_fa>
	<middle_name_fa></middle_name_fa>
	<last_name_fa></last_name_fa>
	<suffix_fa></suffix_fa>
	<email>Ea.educate@liau.ac.ir</email>
	<code>1003194753284600861</code>
	<orcid>1003194753284600861</orcid>
	<coreauthor>Yes
</coreauthor>
	<affiliation>M.Eatemadi,  Department of  Electrical Engineering, Lashtenesha-Zibakenar Branch, Islamic Azad University, Lashtenesha, Iran</affiliation>
	<affiliation_fa></affiliation_fa>
	 </author>


</author_list>


	</article>
</articleset>
</journal>
