Proceedings of the 2015 International Conference on Industrial Technology and Management Science

The Research of Control Technology for Four-rotor Aircraft Based on STM32

Authors
X.Y. Feng, L.L. Yan, C.C. Ji
Corresponding Author
X.Y. Feng
Available Online November 2015.
DOI
https://doi.org/10.2991/itms-15.2015.15How to use a DOI?
Keywords
Four-rotor Aircraft; Attitude Control; Gyroscope; Quaternion; PID
Abstract
The four-rotor aircraft is different from the traditional helicopter. The four-rotor aircraft by changing the speed of the propeller implements various flight movements. According to the characteristics and dynamical features of four-rotor aircraft, this paper mainly studied an attitude control technology of the four-rotor aircraft based on STM32. The three-axis gyroscope and triaxial acceleration sensor of MPU6050 collect the original data, and the data is transmitted to the main controller by I2C. The data with noise is processed by the filter. The stability control problem for the flight attitude of the four-rotor aircraft is solved by using quaternion attitude algorithm, PWM and PID.
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This is an open access article distributed under the CC BY-NC license.

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Proceedings
2015 International Conference on Industrial Technology and Management Science
Part of series
Advances in Computer Science Research
Publication Date
November 2015
ISBN
978-94-6252-123-0
ISSN
2352-538X
DOI
https://doi.org/10.2991/itms-15.2015.15How to use a DOI?
Open Access
This is an open access article distributed under the CC BY-NC license.

Cite this article

TY  - CONF
AU  - X.Y. Feng
AU  - L.L. Yan
AU  - C.C. Ji
PY  - 2015/11
DA  - 2015/11
TI  - The Research of Control Technology for Four-rotor Aircraft Based on STM32
BT  - 2015 International Conference on Industrial Technology and Management Science
PB  - Atlantis Press
SN  - 2352-538X
UR  - https://doi.org/10.2991/itms-15.2015.15
DO  - https://doi.org/10.2991/itms-15.2015.15
ID  - Feng2015/11
ER  -