Attitude solver algorithm based on MUP6050 and HMC5883L
Ji Jin, Hongfei Wang, Donghui Liu, Xue Du
Available Online March 2016.
- https://doi.org/10.2991/icmmct-16.2016.203How to use a DOI?
- attitude solver algorithm,MUP6050,HMC5883L,aircraft control
- 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.
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 -