Authors :
Malothu Kirankumar; Rayudu Santhoshchandra; R. Uday Kumar
Volume/Issue :
Volume 8 - 2023, Issue 1 - January
Google Scholar :
https://bit.ly/3IIfn9N
Scribd :
https://bit.ly/3H6L6CD
DOI :
https://doi.org/10.5281/zenodo.7568657
Abstract :
A quadcopter is one of the most versatile
unmanned aerial vehicles (UAV) used for a variety of
tasks. Quadcopters are symmetrical and use the simplest
principle of operation for controlling roll, pitch, yaw,
and motion. A DJI F450 quadcopter frame design with
optimized geometry is used in this project.All the frame's
components were designed using Fusion 360.Based on
the results of stress analysis with Fusion 360, the
proposed design is validated for its feasibility, and a
suitable material for fabrication is selected through
comparison with five other materials.In this paper, we
investigate the static stress in the quadcopter frame and
the modal frequencies in the quadcopter arm.
Keywords :
Quadcopter, Static Structural, Constraints, Structural Geometry, Design, Analysis, Modal Frequencies, Unmanned Aerial Vehicles
A quadcopter is one of the most versatile
unmanned aerial vehicles (UAV) used for a variety of
tasks. Quadcopters are symmetrical and use the simplest
principle of operation for controlling roll, pitch, yaw,
and motion. A DJI F450 quadcopter frame design with
optimized geometry is used in this project.All the frame's
components were designed using Fusion 360.Based on
the results of stress analysis with Fusion 360, the
proposed design is validated for its feasibility, and a
suitable material for fabrication is selected through
comparison with five other materials.In this paper, we
investigate the static stress in the quadcopter frame and
the modal frequencies in the quadcopter arm.
Keywords :
Quadcopter, Static Structural, Constraints, Structural Geometry, Design, Analysis, Modal Frequencies, Unmanned Aerial Vehicles
