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...
Main Authors: | , , |
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Format: | Article |
Language: | English |
Published: |
Indonesian Institute of Sciences
2014-12-01
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Series: | Journal of Mechatronics, Electrical Power, and Vehicular Technology |
Subjects: | |
Online Access: | http://mevjournal.com/index.php/mev/article/view/178 |