Scholarlink

The design of quadcopters, which are essential to many industries, requires improvements in weight optimisation, structural integrity, and aerodynamic efficiency. We achieved this by developing a novel frame that prioritises strength-to-weight ratio and structural performance through iterative design and simulation. The true X-design was selected for stability and manoeuvrability, supported by material analysis that favours carbon fibre due to its exceptional properties. System simulation, specifically finite element analysis (FEA) using Fusion 360, provided insights into structural integrity. Results validated the frame’s dependability under thrust produced by the drone motors. Our study highlights the significance of novel design and simulation methods in improving quadcopter performance and advancing aerial robotics.

错误：搜索内容不能为空，请输入英文关键词
错误：关键词超出字数限制，请精简
高级检索

Design and Structural Analysis of an Innovative Quadcopter Frame

  • 会议论文

  • 发表日期：

    2025年

查看全文
  • Nobendu Sen,
  • R. Ajith Raj,
  • J. Saji Soundara Raj,
  • Shamim Ibrahim

摘要

The design of quadcopters, which are essential to many industries, requires improvements in weight optimisation, structural integrity, and aerodynamic efficiency. We achieved this by developing a novel frame that prioritises strength-to-weight ratio and structural performance through iterative design and simulation. The true X-design was selected for stability and manoeuvrability, supported by material analysis that favours carbon fibre due to its exceptional properties. System simulation, specifically finite element analysis (FEA) using Fusion 360, provided insights into structural integrity. Results validated the frame’s dependability under thrust produced by the drone motors. Our study highlights the significance of novel design and simulation methods in improving quadcopter performance and advancing aerial robotics.