Experimental Comparison of Hydrogen Fuel Cells and Li-Po Batteries for UAV Endurance

A 300 W air-cooled PEM fuel cell was integrated into a 450 mm quadcopter and its performance was compared to a conventional lithium-polymer battery. The dataset likely contains experimental measurements of voltage, current, power, and temperature under idle and various load conditions. The research was authored by Kirubadurai B and last updated on 2026-05-30.

Use Cases

• Benchmarking fuel cell voltage stability against batteries based on the described steady 12.5 V output.
• Modeling UAV power system performance under dynamic loads based on the described motor throttling and current density data.
• Analyzing thermal management for UAV power systems based on the described temperature rise from 25°C to 40°C.
• Comparing energy source endurance for specific applications based on the described flight duration limitations.

Strengths

• Includes specific performance metrics such as a steady voltage output of 12.5 V and a current under 4.6A.
• Provides a direct comparison between a 300 W PEMFC and a Li-Po battery for a defined 450 mm quadcopter platform.
• Contains detailed experimental observations like a voltage drop from 35.6 V to 32.2 V in the polarization curve.

Limitations

• Column-level documentation is absent; field semantics must be inferred after download.
• Row count is unknown, which may limit suitability assessment.
• The primary data file is a 1.9 MB DOCX document, which may require extraction or conversion for analysis.

Provenance

Source

figshare

Collection Method

Experimental integration and testing of a PEM fuel cell in a quadcopter.

Freshness

Last updated 2026-05-30 10:24:52; freshness should be verified.