Attitude solver algorithm based on MUP6050 and HMC5883L

DOI

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.

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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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  - 10.2991/icmmct-16.2016.203
ID  - Jin2016/03
ER  -