Paper Title:
A Study on Information Fusion of AHRS Based on DSP
  Abstract

For the angular velocity gyro drift and noise and the inertial navigation solution of the integral nature, the navigation error of the attitude will accumulate over time. With the increase of navigation time, the system may fail. In high dynamic motion the accelerometer / magnetometer attitude measurement navigation system will not work properly. Therefore, the accelerometer / magnetometer attitude determination system, haven’t no drift, but poor dynamic performance. This article will realize a low-cost, precision Attitude Calculation System with more effective integration of the two.

  Info
Periodical
Advanced Materials Research (Volumes 271-273)
Edited by
Junqiao Xiong
Pages
802-807
DOI
10.4028/www.scientific.net/AMR.271-273.802
Citation
H. S. Tan, X. M. Yuan, J. H. Zhu, "A Study on Information Fusion of AHRS Based on DSP", Advanced Materials Research, Vols. 271-273, pp. 802-807, 2011
Online since
July 2011
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Price
$32.00
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