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:: دوره 7، شماره 1 - ( 10-1395 ) ::
جلد 7 شماره 1 صفحات 77-85 برگشت به فهرست نسخه ها
Mathematical Dynamics, Kinematics Modeling and PID Equation Controller Of QuadCopter
چکیده:   (2935 مشاهده)
Abstract 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  the Dynamics and Kinematics model of  quadcopter  and the effect of forces by introducing two frames on the ground and it’s body, also we design and implement the PID controller then found the best way of manual tuning for adjusting the PID  coefficient  in  Symmetric quadcopter , we use the 10 DOF IMU consist of  three axis gyroscope ,accelerometer and magnetometer with three PID  controller for Roll, Pitch, Yaw angle and the separate PID  controller for altitude of quadcopter Robot, also build it based on extracted result. 
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نوع مطالعه: كاربردي | موضوع مقاله: تخصصي
دریافت: 1395/6/24 | پذیرش: 1396/9/28 | انتشار: 1396/9/28
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Etemadi M. Mathematical Dynamics, Kinematics Modeling and PID Equation Controller Of QuadCopter. International Journal of Applied Operational Research. 2017; 7 (1) :77-85
URL: http://ijorlu.liau.ac.ir/article-1-503-fa.html

Mathematical Dynamics, Kinematics Modeling and PID Equation Controller Of QuadCopter. ژورنال بین المللی پژوهش عملیاتی. 1395; 7 (1) :77-85

URL: http://ijorlu.liau.ac.ir/article-1-503-fa.html



دوره 7، شماره 1 - ( 10-1395 ) برگشت به فهرست نسخه ها
ژورنال بین المللی پژوهش عملیاتی International Journal of Applied Operational Research - An Open Access Journal
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