China Aerospace Science and Industry Corporation (CASIC) - Unscented Kalman filter for SINS alignment

Author(s): Zhou Zhanxin ; Gao Yanan ; Chen Liabin
Publisher: China Aerospace Science and Industry Corporation (CASIC)
Publication Date: 1 June 2007
Volume: 18
Page(s): 327 - 333
ISSN (Electronic): 1004-4132
DOI: 10.1016/S1004-4132(07)60094-2
Regular:

In order to improve the filter accuracy for the nonlinear error model of strapdown inertial navigation system (SINS) alignment, Unscented Kalman Filter (UKF) is presented for simulation with... View More

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