Implementation of Hexacopter for Package Delivery
This paper presents the engineering design of an unmanned aerial vehicle (UAV)/drone hexacopter and optimizes the PID (Proportional-Integral-Derivate) values for the Pixhawk 2.4.8 (PX4) flight controller. The design phase begins with component selection and identification, with the goal that the dro...
| Published in: | Majlesi Journal of Electrical Engineering |
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| Format: | Article |
| Language: | English |
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Islamic Azad University
2024
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| Online Access: | https://www.scopus.com/inward/record.uri?eid=2-s2.0-85194967904&doi=10.30486%2fmjee.2024.1991363.1177&partnerID=40&md5=e3d4a2e60bff5e3081d50c57b622d590 |
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2-s2.0-85194967904 Suparta W.; Ahmad A.C.; Tharim A.H.A. Implementation of Hexacopter for Package Delivery 2024 Majlesi Journal of Electrical Engineering 18 1 10.30486/mjee.2024.1991363.1177 https://www.scopus.com/inward/record.uri?eid=2-s2.0-85194967904&doi=10.30486%2fmjee.2024.1991363.1177&partnerID=40&md5=e3d4a2e60bff5e3081d50c57b622d590 This paper presents the engineering design of an unmanned aerial vehicle (UAV)/drone hexacopter and optimizes the PID (Proportional-Integral-Derivate) values for the Pixhawk 2.4.8 (PX4) flight controller. The design phase begins with component selection and identification, with the goal that the drone can carry loads up to 3 kg. Then install the main components and test the construction results. An analysis of the experimental results of the PID PX4 controller with no load and with load was performed. Results from direct field experiments with a home-built hexacopter show that the default PID must be tuned to be able to lift a load with a specific target. © The Author(s) 2024 Islamic Azad University 2345377X English Article |
| author |
Suparta W.; Ahmad A.C.; Tharim A.H.A. |
| spellingShingle |
Suparta W.; Ahmad A.C.; Tharim A.H.A. Implementation of Hexacopter for Package Delivery |
| author_facet |
Suparta W.; Ahmad A.C.; Tharim A.H.A. |
| author_sort |
Suparta W.; Ahmad A.C.; Tharim A.H.A. |
| title |
Implementation of Hexacopter for Package Delivery |
| title_short |
Implementation of Hexacopter for Package Delivery |
| title_full |
Implementation of Hexacopter for Package Delivery |
| title_fullStr |
Implementation of Hexacopter for Package Delivery |
| title_full_unstemmed |
Implementation of Hexacopter for Package Delivery |
| title_sort |
Implementation of Hexacopter for Package Delivery |
| publishDate |
2024 |
| container_title |
Majlesi Journal of Electrical Engineering |
| container_volume |
18 |
| container_issue |
1 |
| doi_str_mv |
10.30486/mjee.2024.1991363.1177 |
| url |
https://www.scopus.com/inward/record.uri?eid=2-s2.0-85194967904&doi=10.30486%2fmjee.2024.1991363.1177&partnerID=40&md5=e3d4a2e60bff5e3081d50c57b622d590 |
| description |
This paper presents the engineering design of an unmanned aerial vehicle (UAV)/drone hexacopter and optimizes the PID (Proportional-Integral-Derivate) values for the Pixhawk 2.4.8 (PX4) flight controller. The design phase begins with component selection and identification, with the goal that the drone can carry loads up to 3 kg. Then install the main components and test the construction results. An analysis of the experimental results of the PID PX4 controller with no load and with load was performed. Results from direct field experiments with a home-built hexacopter show that the default PID must be tuned to be able to lift a load with a specific target. © The Author(s) 2024 |
| publisher |
Islamic Azad University |
| issn |
2345377X |
| language |
English |
| format |
Article |
| accesstype |
|
| record_format |
scopus |
| collection |
Scopus |
| _version_ |
1809678010980237312 |