Design and Analysis of a Micro Class UAV Integrating Zimmerman Configuration
Authors : K Harshavardhan; AM Sanjana; P Shyam Raja; Dileshwar Rao; A Neha; P Karthik Reddy; J H S D Anoohya
Volume/Issue : Volume 9 - 2024, Issue 3 - March
Google Scholar : https://tinyurl.com/59efjxvk
Scribd : https://tinyurl.com/mtbxeuje
DOI : https://doi.org/10.38124/ijisrt/IJISRT24MAR1051
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Abstract : This document describes the design and analysis processes followed by team to build a micro class UAV. Through this opportunity our team has gotten a chance to test and enhance our skills by developing a design and fabricate flying wing UAV of Zimmerman configuration. Integrating this flying wing into the blended body micro classed UAV, allowed the team members to push limits further and work extra hard to make the ends meet, with the final design of a lightweight UAV following all the constrains for the SAE ADC 2020.
Keywords : UAV; Zimmerman; Lightweight.
Keywords : UAV; Zimmerman; Lightweight.