Design and Static Structural Analysis of Plus Configuration Octa-copter |
Author(s): |
| Santosh Yadav , East West College of Engineering; Ashwini N, east west college of engineering; Lalitha R, east west college of engineering; Ranjitha V, east west college of engineering; J K Bhushan, east west college of engineering |
Keywords: |
| Octa-copter, Stress, Displacement, ANSYS, CATIA, Static Analysis |
Abstract |
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There are various requirements which should be satisfied by the structure and is best rigid body as light as possible, capability of carrying heavy payload, mounting the electronics components such as sensor, ESC, motor etc., which can be achieved by the various modification & optimization of various structural parameters, structural design and analysis of multi-rotor for integration into whole system for the best result. Design of a novel acrobatic holonomic multi-copter UAV is carried out using CAE tools to produce desired design concept. Analysis of multi-copter is executed using analysis tools. By design optimization; number of motors, type of propeller & design of airframe has been sketched conceptually. In this type of drone, payload weight is an important factor which have been taken into consideration. |
Other Details |
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Paper ID: IJSRDV7I90010 Published in: Volume : 7, Issue : 9 Publication Date: 01/12/2019 Page(s): 520-522 |
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