The Design of Quadcopter Frame Based On Finite Element Analysis
Pan Wei, Zijian Yang, Quanzi Wang
Available Online April 2015.
- https://doi.org/10.2991/icmra-15.2015.260How to use a DOI?
- Quadcopter Ansys Static and model analysis
- The frame is an important basis for aircraft structural the design improvements and innovation as a whole frame bearing member. Early in the design stage, a large number of samples are used in the collision and reliability test, which not only causes a waste of resources, but also puts a lot of manpower and resources. So the development cycle is quite lengthy. With the continuing development of computer technology and scientific calculations, the introduction of the finite element method greatly shorten the development cycle frame. More and more machinery and aerospace companies have seen finite element structural analysis as a necessary part of the mechanical development. Using the finite element method, optimization of key parts of the machine and the machine has become an indispensable part of the development process. This paper will analyze the static and modal frame, in order to reflect the important role of finite element analysis in the frame design.
- Open Access
- This is an open access article distributed under the CC BY-NC license.
Cite this article
TY - CONF AU - Pan Wei AU - Zijian Yang AU - Quanzi Wang PY - 2015/04 DA - 2015/04 TI - The Design of Quadcopter Frame Based On Finite Element Analysis BT - Proceedings of the 3rd International Conference on Mechatronics, Robotics and Automation PB - Atlantis Press SP - 1353 EP - 1356 SN - 2352-538X UR - https://doi.org/10.2991/icmra-15.2015.260 DO - https://doi.org/10.2991/icmra-15.2015.260 ID - Wei2015/04 ER -