Open Access
2014 An Aeromagnetic Compensation Algorithm for Aircraft Based on Fuzzy Adaptive Kalman Filter
Yao Zhang, Yu-Xin Zhao, Shuai Chang
J. Appl. Math. 2014(SI23): 1-9 (2014). DOI: 10.1155/2014/405671

Abstract

In order to ensure the effectiveness of geomagnetic navigation, as the foundation, the precise measurement of geomagnetic field must be guaranteed; namely, aircraft aeromagnetic compensation is worthy of being further studied. In this paper, the classical aircraft aeromagnetic compensation algorithm based on Leliak Model is analyzed and an aircraft aeromagnetic compensation algorithm based on fuzzy adaptive Kalman filter is proposed, which is a new approach for aircraft to achieve aeromagnetic compensation. Simulation results show that it has better compensation performance without relying on the aircraft attitude.

Citation

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Yao Zhang. Yu-Xin Zhao. Shuai Chang. "An Aeromagnetic Compensation Algorithm for Aircraft Based on Fuzzy Adaptive Kalman Filter." J. Appl. Math. 2014 (SI23) 1 - 9, 2014. https://doi.org/10.1155/2014/405671

Information

Published: 2014
First available in Project Euclid: 27 February 2015

zbMATH: 07131575
Digital Object Identifier: 10.1155/2014/405671

Rights: Copyright © 2014 Hindawi

Vol.2014 • No. SI23 • 2014
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