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

DOI

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.

Copyright

© 2015, 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  - 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  - Proceedings of the 2015 International Conference on Industrial Technology and Management Science
PB  - Atlantis Press
SP  - 58
EP  - 61
SN  - 2352-538X
UR  - https://doi.org/10.2991/itms-15.2015.15
DO  - 10.2991/itms-15.2015.15
ID  - Feng2015/11
ER  -