Proceedings of the 2016 4th International Conference on Machinery, Materials and Computing Technology

Attitude solver algorithm based on MUP6050 and HMC5883L

Authors
Ji Jin, Hongfei Wang, Donghui Liu, Xue Du
Corresponding Author
Ji Jin
Available Online March 2016.
DOI
https://doi.org/10.2991/icmmct-16.2016.203How to use a DOI?
Keywords
attitude solver algorithm,MUP6050,HMC5883L,aircraft control
Abstract
In aircraft control, getting the current aircraft attitude is foundation that we can control the flight of aircraft.In this paper,MUP6050 and HMC5883L sensors are used to measure aircraft attitude.As time goes on,the accumulation of integral error is growing,when the gyroscope is used to solver aircraft attitude;In the static,we can receive relatively stable attitude,but in large acceleration,the attitude will be interfered by large acceleration,when using accelerometer solver; Accuracy of attitude data be lost in strong magnetic of motor,when using the electronic compass solver.Data of gyroscope, accelerometer and electronic compass is used to solver attitude by Interpolation method in this paper.
Open Access
This is an open access article distributed under the CC BY-NC license.

Download article (PDF)

Volume Title
Proceedings of the 2016 4th International Conference on Machinery, Materials and Computing Technology
Series
Advances in Engineering Research
Publication Date
March 2016
ISBN
978-94-6252-165-0
ISSN
2352-5401
DOI
https://doi.org/10.2991/icmmct-16.2016.203How 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  - Ji Jin
AU  - Hongfei Wang
AU  - Donghui Liu
AU  - Xue Du
PY  - 2016/03
DA  - 2016/03
TI  - Attitude solver algorithm based on MUP6050 and HMC5883L
BT  - Proceedings of the 2016 4th International Conference on Machinery, Materials and Computing Technology
PB  - Atlantis Press
SP  - 1025
EP  - 1029
SN  - 2352-5401
UR  - https://doi.org/10.2991/icmmct-16.2016.203
DO  - https://doi.org/10.2991/icmmct-16.2016.203
ID  - Jin2016/03
ER  -