Application of Improved Adaptive UKF Algorithm on Aircraft Attitude Estimation System

DOI

10.2991/isrme-15.2015.203How to use a DOI?

Keywords

Adaptive; UKF; aircraft attitude estimation; estimation accuracy

Abstract

For the problem of aircraft attitude estimation system, Unscented Kalman Filter (UKF) algorithm is easy to be disturbed. Therefore, an improved adaptive UKF algorithm which can overcome disturbance well by introducing adaptive factors to adjust the state gain matrix is proposed in this paper. The simulation results show the effectiveness of the proposed algorithm.

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  - Jun-hui Zheng
AU  - Fei-fei Ning
PY  - 2015/04
DA  - 2015/04
TI  - Application of Improved Adaptive UKF Algorithm on Aircraft Attitude Estimation System
BT  - Proceedings of the 2015 International Conference on Intelligent Systems Research and Mechatronics Engineering
PB  - Atlantis Press
SP  - 976
EP  - 979
SN  - 1951-6851
UR  - https://doi.org/10.2991/isrme-15.2015.203
DO  - 10.2991/isrme-15.2015.203
ID  - Zheng2015/04
ER  -