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...
Saved in:
| Main Authors: | , , |
|---|---|
| Format: | Article |
| Language: | English |
| Published: |
OICC Press
2024-04-01
|
| Series: | Majlesi Journal of Electrical Engineering |
| Subjects: | |
| Online Access: | https://oiccpress.com/mjee/article/view/5053 |
| Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
| _version_ | 1849414957877166080 |
|---|---|
| author | Wayan Suparta Asmalia Che Ahmad Asniza Hamimi Abdul Tharim |
| author_facet | Wayan Suparta Asmalia Che Ahmad Asniza Hamimi Abdul Tharim |
| author_sort | Wayan Suparta |
| collection | DOAJ |
| 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.
|
| format | Article |
| id | doaj-art-bade1b69609e43fa9c9abca3bee97161 |
| institution | Kabale University |
| issn | 2345-377X 2345-3796 |
| language | English |
| publishDate | 2024-04-01 |
| publisher | OICC Press |
| record_format | Article |
| series | Majlesi Journal of Electrical Engineering |
| spelling | doaj-art-bade1b69609e43fa9c9abca3bee971612025-08-20T03:33:39ZengOICC PressMajlesi Journal of Electrical Engineering2345-377X2345-37962024-04-0118110.30486/mjee.2024.1991363.1177Implementation of Hexacopter for Package DeliveryWayan SupartaAsmalia Che AhmadAsniza Hamimi Abdul TharimThis 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. https://oiccpress.com/mjee/article/view/5053Delivery PackagesHexacopter DronePID Controller TuningPixhawk 2.4.8 |
| spellingShingle | Wayan Suparta Asmalia Che Ahmad Asniza Hamimi Abdul Tharim Implementation of Hexacopter for Package Delivery Majlesi Journal of Electrical Engineering Delivery Packages Hexacopter Drone PID Controller Tuning Pixhawk 2.4.8 |
| title | 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_short | Implementation of Hexacopter for Package Delivery |
| title_sort | implementation of hexacopter for package delivery |
| topic | Delivery Packages Hexacopter Drone PID Controller Tuning Pixhawk 2.4.8 |
| url | https://oiccpress.com/mjee/article/view/5053 |
| work_keys_str_mv | AT wayansuparta implementationofhexacopterforpackagedelivery AT asmaliacheahmad implementationofhexacopterforpackagedelivery AT asnizahamimiabdultharim implementationofhexacopterforpackagedelivery |