A Constant Voltage/Current CPT System With Lightweight Characteristics for the Unmanned Aerial Vehicle

The large weight of the unmanned aerial vehicle (UAV) could cause a decrease in endurance mileage, while poor anti-offset performance could extend charging time and may even damage onboard equipment. To address the above issues in constant-voltage/current capacitive power transfer (CPT) system for t...

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Bibliographic Details
Main Authors: Yufang Chang, Xiaoke Zhang, Chao Ma, Wencong Huang, Huaicheng Yan
Format: Article
Language:English
Published: IEEE 2024-01-01
Series:IEEE Access
Subjects:
Online Access:https://ieeexplore.ieee.org/document/10375494/
Description
Summary:The large weight of the unmanned aerial vehicle (UAV) could cause a decrease in endurance mileage, while poor anti-offset performance could extend charging time and may even damage onboard equipment. To address the above issues in constant-voltage/current capacitive power transfer (CPT) system for the UAV, a constant voltage/current (CV/CC) CPT system with lightweight characteristics for the UAV is proposed. Firstly, a capacitive coupler with strong anti-offset tolerance for the CPT system is proposed, and the coupling performance and equivalent model are studied. Secondly, the switching strategy for constant voltage/current output is studied based on the T-<inline-formula> <tex-math notation="LaTeX">$\pi $ </tex-math></inline-formula> type compensation circuit, without additional compensating elements. Finally, a simulation model and a test prototype are built to verify the feasibility and effectiveness of the proposed system. The results show that the system achieved a constant voltage output of 60 V and a constant current output of 2 A. And the rate of change of the output voltage and current is less than 6&#x0025; when the capacitive coupler is offset by &#x00B1;100 mm, the rate of that is less than 6&#x0025; when the load changes. The switching strategy proposed in this paper has obvious lightweight advantages and could serve as a reference for designing the CPT system for the UAV.
ISSN:2169-3536