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@article{187102,
author = {Abhay P and Bhuvan M S and Bhanuprakash and Akasha and Asst Professor Nataraja N and Asst Professor Niveditha V K},
title = {Design, Performance, and Regulatory Considerations for Payload Drones: A Comprehensive Study},
journal = {International Journal of Innovative Research in Technology},
year = {2025},
volume = {12},
number = {6},
pages = {3275-3278},
issn = {2349-6002},
url = {https://ijirt.org/article?manuscript=187102},
abstract = {With an emphasis on design trade-offs, payload integration methodologies, performance characterization, safety and regulatory limitations and application scenarios (medical logistics, last-mile commerce, and disaster response), this article examines payload-capable unmanned aerial vehicles (UAVs). We conduct mixed-methods research that includes a policy examination of airworthiness and operational constraints, bench and flight testing of modular payload racks (0.5-8 kg range) and a technical design analysis. These are our goals: (1) to measure the effects of incremental payload mass and center-of-gravity changes on flight stability and endurance (2) to assess medical and commercial products payload release and securement systems; and (3) to compile regulatory requirements that impact payload operations. The findings will provide a standard test procedure for payload performance and safety certification, as well as design requirements for medium lift delivery drones (payload = 0.5-8 kg). Important conclusions from the literature and industry practice show that feasible payload mass and operating envelope are significantly determined by mission profile, national regulations and payload design (external vs. embedded).},
keywords = {payload drone, UAV payload, payload capacity, drone delivery, regulatory framework, DGCA, flight-testing},
month = {November},
}
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