Paper Title:
Attitude Resolution Algorithm of Gyro-Free Inertial Navigation System
  Abstract

Gyro-Free Inertial Navigation System(GFINS) is constructed mainly with accelerometers. A nine-accelerometer GFINS scheme is designed and the prototype is manufactured. Then quaternion based attitude resolution algorithm is developed, the algorithm is also applied to the GFINS prototype, the results show that the algorithm can effectively offspring the cone-effect, and the attitude is resolute validly, the maximum attitude error is up to 0.37°, the maximum azimuth error is 0.47°.

  Info
Periodical
Advanced Materials Research (Volumes 308-310)
Chapter
Product Life Cycle Design
Edited by
Jian Gao
Pages
662-667
DOI
10.4028/www.scientific.net/AMR.308-310.662
Citation
H. G. Zhou, X. S. Wang, C. T. Yi, "Attitude Resolution Algorithm of Gyro-Free Inertial Navigation System", Advanced Materials Research, Vols. 308-310, pp. 662-667, 2011
Online since
August 2011
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Price
$32.00
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