Propeller Speed Control System on Autonomous Quadcopter with Variations in Load Fulcrum Point

The need for unmanned vehicles is increasingly needed in certain conditions, such as distribution of disaster supply, distribution of medicines, distribution of vaccines in the affected areas in pandemic situations. The various types of goods to be distributed require a different fulcrum. This resea...

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Autores principales:	Ratna Aisuwarya, Ibrahim Saputra, Dodon Yendri
Formato:	article
Lenguaje:	ID
Publicado:	Universitas Udayana 2021
Materias:	Electronic computers. Computer science QA75.5-76.95
Acceso en línea:	https://doaj.org/article/c9b6c4396325472ca688c41e8f66985f
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id	oai:doaj.org-article:c9b6c4396325472ca688c41e8f66985f
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spelling	oai:doaj.org-article:c9b6c4396325472ca688c41e8f66985f2021-12-01T04:18:06ZPropeller Speed Control System on Autonomous Quadcopter with Variations in Load Fulcrum Point2088-15412541-583210.24843/LKJITI.2021.v12.i03.p04https://doaj.org/article/c9b6c4396325472ca688c41e8f66985f2021-11-01T00:00:00Zhttps://ojs.unud.ac.id/index.php/lontar/article/view/77557https://doaj.org/toc/2088-1541https://doaj.org/toc/2541-5832The need for unmanned vehicles is increasingly needed in certain conditions, such as distribution of disaster supply, distribution of medicines, distribution of vaccines in the affected areas in pandemic situations. The various types of goods to be distributed require a different fulcrum. This research implemented PID control for the quadcopter balance control system to achieve stability during hovering. PID control is used to achieve a certain setpoint to produce the required PWM output for the propeller to reach a speed that can fly the quadcopter tilted until it reaches a steady state. Tests were carried out on the roll and pitch motion of the quadcopter by providing a load. The results show that PID control can be implemented for the quadcopter balance control system during hovering by determining the PID constants for each roll and pitch motion with the constanta of Kp = 0.15, Kd = 0.108, and Ki = 0.05. The quadcopter takes 3 – 6 seconds to return to the 0 degree setpoint when it is loaded.Ratna AisuwaryaIbrahim SaputraDodon YendriUniversitas UdayanaarticleElectronic computers. Computer scienceQA75.5-76.95IDLontar Komputer, Vol 12, Iss 3, Pp 163-174 (2021)
institution	DOAJ
collection	DOAJ
language	ID
topic	Electronic computers. Computer science QA75.5-76.95
spellingShingle	Electronic computers. Computer science QA75.5-76.95 Ratna Aisuwarya Ibrahim Saputra Dodon Yendri Propeller Speed Control System on Autonomous Quadcopter with Variations in Load Fulcrum Point
description	The need for unmanned vehicles is increasingly needed in certain conditions, such as distribution of disaster supply, distribution of medicines, distribution of vaccines in the affected areas in pandemic situations. The various types of goods to be distributed require a different fulcrum. This research implemented PID control for the quadcopter balance control system to achieve stability during hovering. PID control is used to achieve a certain setpoint to produce the required PWM output for the propeller to reach a speed that can fly the quadcopter tilted until it reaches a steady state. Tests were carried out on the roll and pitch motion of the quadcopter by providing a load. The results show that PID control can be implemented for the quadcopter balance control system during hovering by determining the PID constants for each roll and pitch motion with the constanta of Kp = 0.15, Kd = 0.108, and Ki = 0.05. The quadcopter takes 3 – 6 seconds to return to the 0 degree setpoint when it is loaded.
format	article
author	Ratna Aisuwarya Ibrahim Saputra Dodon Yendri
author_facet	Ratna Aisuwarya Ibrahim Saputra Dodon Yendri
author_sort	Ratna Aisuwarya
title	Propeller Speed Control System on Autonomous Quadcopter with Variations in Load Fulcrum Point
title_short	Propeller Speed Control System on Autonomous Quadcopter with Variations in Load Fulcrum Point
title_full	Propeller Speed Control System on Autonomous Quadcopter with Variations in Load Fulcrum Point
title_fullStr	Propeller Speed Control System on Autonomous Quadcopter with Variations in Load Fulcrum Point
title_full_unstemmed	Propeller Speed Control System on Autonomous Quadcopter with Variations in Load Fulcrum Point
title_sort	propeller speed control system on autonomous quadcopter with variations in load fulcrum point
publisher	Universitas Udayana
publishDate	2021
url	https://doaj.org/article/c9b6c4396325472ca688c41e8f66985f
work_keys_str_mv	AT ratnaaisuwarya propellerspeedcontrolsystemonautonomousquadcopterwithvariationsinloadfulcrumpoint AT ibrahimsaputra propellerspeedcontrolsystemonautonomousquadcopterwithvariationsinloadfulcrumpoint AT dodonyendri propellerspeedcontrolsystemonautonomousquadcopterwithvariationsinloadfulcrumpoint
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Propeller Speed Control System on Autonomous Quadcopter with Variations in Load Fulcrum Point

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