Implementation of Hexacopter for Package Delivery

Publish Year: 1403
نوع سند: مقاله ژورنالی
زبان: English
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شناسه ملی سند علمی:

JR_MJEE-18-1_018

تاریخ نمایه سازی: 9 اردیبهشت 1403

Abstract:

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 ۲.۴.۸ (PX۴) flight controller. The design phase begins with component selection and identification, with the goal that the drone can carry loads up to ۳ kg. Then install the main components and test the construction results. An analysis of the experimental results of the PID PX۴ 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.

Authors

Wayan Suparta

Department of Electrical Engineering, Institut Teknologi Nasional Yogyakarta, Yogyakarta ۵۵۲۸۱, Indonesia.

Asmalia Ahmad

Department of Built Environment Studies and Technology, Faculty of Architecture, Planning and Surveying, Universiti Teknologi MARA (UiTM), Perak Branch, Malaysia

Asniza Abdul Tharim

Department of Built Environment Studies and Technology, Faculty of Architecture, Planning and Surveying, Universiti Teknologi MARA, Perak Branch, Malaysia

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