Flight Test of the Quadrotor based on Algorithm of Multi-sensor Fusion

DOI

10.2991/itoec-16.2016.61How to use a DOI?

Keywords

Kalman filter; integrated navigation system; flight test

Abstract

This paper introduces a multi-sensor fusion technology and verify Whether the integrated navigation system is valid. IMU and GPS/ barometer is complementary, the former's long-term stability is poor and short-term stability is good, and the latter is just the opposite. Therefore, the fusion algorithm can be used to combine the three data, the output of three-dimensional position information, speed information, attitude information, to provide navigation information for quadrotor. In loiter mode, fluctuations of roll channel and elevation channel are reduced, height tracking situation is better .

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/).

Download article (PDF)

TY  - CONF
AU  - Lingyu Liu
AU  - Xinhua Wang
AU  - Qingyan Tan
PY  - 2016/05
DA  - 2016/05
TI  - Flight Test of the Quadrotor based on Algorithm of Multi-sensor Fusion
BT  - Proceedings of the 2nd Information Technology and Mechatronics Engineering Conference (ITOEC 2016)
PB  - Atlantis Press
SP  - 323
EP  - 328
SN  - 2352-5401
UR  - https://doi.org/10.2991/itoec-16.2016.61
DO  - 10.2991/itoec-16.2016.61
ID  - Liu2016/05
ER  -