Proceedings of the 2016 3rd International Conference on Materials Engineering, Manufacturing Technology and Control

An Optimized Flight Control System of Quad-rotor Aircraft

Authors
Xiaoning Chen, Hongting Dong, Dexiang Zhang, Jing Xia
Corresponding Author
Xiaoning Chen
Available Online April 2016.
DOI
10.2991/icmemtc-16.2016.198How to use a DOI?
Keywords
optimization;csyncretic data of gyroscope; accelerometer and magnetometer;fuzzy algorithm;joint simulation
Abstract

The flight performance of four-rotor unmanned helicopter depends largely on the flight control system, the flight control system was mainly consisted of attitude algorithm and controller. During design time, firstly, in order to real-time update for the quaternion , we fused the data of gyroscope accelerometer and magnetometer. And we obtained the attitude angle through quaternion to Euler angle conversion. Then, we calculated the output of throttle by fuzzy algorithm, which was used to control the attitude. And control algorithm was used and optimized by the method of the joint simulation. Finally, four-rotor unmanned helicopter was connected to PC with bluetooth and we obtained the air data of UAV form PC. The data display that the fuzzy controller can keep the stability of flying

Copyright
© 2016, 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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Volume Title
Proceedings of the 2016 3rd International Conference on Materials Engineering, Manufacturing Technology and Control
Series
Advances in Engineering Research
Publication Date
April 2016
ISBN
978-94-6252-173-5
ISSN
2352-5401
DOI
10.2991/icmemtc-16.2016.198How to use a DOI?
Copyright
© 2016, 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/).

Cite this article

TY  - CONF
AU  - Xiaoning Chen
AU  - Hongting Dong
AU  - Dexiang Zhang
AU  - Jing Xia
PY  - 2016/04
DA  - 2016/04
TI  - An Optimized Flight Control System of Quad-rotor Aircraft
BT  - Proceedings of the 2016 3rd International Conference on Materials Engineering, Manufacturing Technology and Control
PB  - Atlantis Press
SP  - 1000
EP  - 1003
SN  - 2352-5401
UR  - https://doi.org/10.2991/icmemtc-16.2016.198
DO  - 10.2991/icmemtc-16.2016.198
ID  - Chen2016/04
ER  -