Research on The Principle And Optimization of Multi-Rotor Aircraft

DOI

10.2991/jiaet-18.2018.52How to use a DOI?

Keywords

Steady-state; PID; Regulation of Multi-rotor; Aircraft

Abstract

In today's society, unmanned aerial vehicles are becoming increasingly mature and popularized with each passing day. Compared with other fixed-wing aircraft, helicopter-based aircraft and multi-rotor aircraft have emerged like bamboo shoots because it can vertically take off and land, be easy to manufacture, easy to control, and can complete all kinds of attitude flights. While in multi-rotor aircraft, multi-rotor aircraft with four-axis and even multiples occupy almost 100% of the market. This is because the multi-rotor aircraft of even number times is characterized by easy production, simple principle, and so on. However, if it is not sufficiently optimized in practical application, its anti-jamming ability and adaptability in flight are still not very ideal. In this paper, we will analyze its working principle represented by four axes, and try to further optimize the design of it.

Copyright

© 2018, the Authors. Published by Atlantis Press.

Open Access

This is an open access article distributed under the CC BY-NC license (http://creativecommons.org/licenses/by-nc/4.0/).

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TY  - CONF
AU  - Wei Zhang
AU  - Dongzi Zhao
PY  - 2018/03
DA  - 2018/03
TI  - Research on The Principle And Optimization of Multi-Rotor Aircraft
BT  - Proceedings of the 2018 Joint International Advanced Engineering and Technology Research Conference (JIAET 2018)
PB  - Atlantis Press
SP  - 296
EP  - 301
SN  - 2352-5401
UR  - https://doi.org/10.2991/jiaet-18.2018.52
DO  - 10.2991/jiaet-18.2018.52
ID  - Zhang2018/03
ER  -