Proportional Derivative Active Force Control for “X” Configuration Quadcopter

Proportional Derivative Active Force Control for “X” Configuration Quadcopter

<p>This paper present a control method “x” configuration quadcopter. The control method used PDAFC (Proportional Derivative Active Force Control). PD is used to stabilize quadcopter, and AFC is used to reject uncertainty disturbance (e.g. wind) by estimate disturbance torque value of quadcopte...

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Bibliographic Details
Main Authors: Niam Tamami, Endra Pitowarno, I Gede Puja Astawa
Format: Article
Language:English
Published: Indonesian Institute of Sciences 2014-12-01
Series:Journal of Mechatronics, Electrical Power, and Vehicular Technology
Subjects:
“x”
quadcopter
stability
PD
AFC
Online Access:http://mevjournal.com/index.php/mev/article/view/178

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