BEGIN:VCALENDAR
VERSION:2.0
PRODID:IEEE vTools.Events//EN
CALSCALE:GREGORIAN
BEGIN:VTIMEZONE
TZID:Asia/Karachi
BEGIN:STANDARD
DTSTART:20091031T230000
TZOFFSETFROM:+0600
TZOFFSETTO:+0500
TZNAME:PKT
END:STANDARD
END:VTIMEZONE
BEGIN:VEVENT
DTSTAMP:20160421T142315Z
UID:F2876179-E5B6-11E7-833E-0050568D7F66
DTSTART;TZID=Asia/Karachi:20160420T060000
DTEND;TZID=Asia/Karachi:20160420T073000
DESCRIPTION:IEEE Control Society Islamabad has organized an event on &quot;Nonli
 near Control of Helicopter Model using Sliding Mode Control&quot; on 20th April
 \, 2016 at Capital University of Science and Technology (CUST).\n\nHelicop
 ter is a mechanical system used for flying purpose having many flying feat
 ures. It offer a challenging task to design a controller for helicopters s
 tability control. This helicopter model will be used to implement a simula
 tion environment that can give a valid alternative to real flight testing.
  When the simulation environment is in place\, the task is to develop a co
 ntroller that will stabilize the helicopter.\n\nThe CE 150 is a helicopter
  model intended to study dynamics of this system and apply control systems
  techniques. In the First part\, helicopter model is described\, followed 
 by mathematical modeling. In next part\, model simulation results without 
 controller are explained. First order and higher order Sliding Mode contro
 ller are applied and their results have been compared to show the removal 
 of chattering by higher order sliding mode controller. Only elevation dyna
 mics of model helicopter are used in this document to consider a system fr
 ee of cross coupling.\n\nCo-sponsored by: Capital University of Science an
 d Technology\, Islamabad\n\nSpeaker(s): Raheel Anjum\, \n\nIslamabad\, Isl
 amabad Capital Territory\, Pakistan
LOCATION:Islamabad\, Islamabad Capital Territory\, Pakistan
ORGANIZER:aib@jinnah.edu.pk
SEQUENCE:0
SUMMARY:[Legacy Report] Nonlinear Control of Helicopter Model using Sliding
  Mode Control
URL;VALUE=URI:https://events.vtools.ieee.org/m/133680
X-ALT-DESC:Description: &lt;br /&gt;&lt;p&gt;IEEE Control Society Islamabad has organiz
 ed an event on &quot;&lt;strong&gt;&lt;strong&gt;&lt;strong&gt;&lt;strong&gt;&lt;strong&gt;Nonlinear Control 
 of Helicopter Model using Sliding Mode Control&lt;/strong&gt;&lt;/strong&gt;&lt;/strong&gt;&lt;
 /strong&gt;&lt;/strong&gt;&quot; on 20th April\, 2016 at Capital University of Science a
 nd Technology (CUST).&lt;/p&gt;\n&lt;p&gt;Helicopter is a mechanical system used for f
 lying purpose having many flying features. It offer a challenging task to 
 design a controller for helicopters stability control. This helicopter mod
 el will be used to implement a simulation environment that can give a vali
 d alternative to real flight testing. When the simulation environment is i
 n place\, the task is to develop a controller that will stabilize the heli
 copter.&lt;/p&gt;\n&lt;p&gt;The CE 150 is a helicopter model intended to study dynamic
 s of this system and apply control systems techniques. In the First part\,
  helicopter model is described\, followed by mathematical modeling.&amp;nbsp\;
  In next part\, model simulation results without controller are explained.
  First order and higher order Sliding Mode controller are applied and thei
 r results have been compared to show the removal of chattering by higher o
 rder sliding mode controller. Only elevation dynamics of model helicopter 
 are used in this document to consider a system free of cross coupling.&lt;/p&gt;
END:VEVENT
END:VCALENDAR