Title of article
Improved self-alignment scheme for SINS using augmented measurement
Author/Authors
Acharya، نويسنده , , Arunasish and Sadhu، نويسنده , , Smita and Ghoshal، نويسنده , , T.K.، نويسنده ,
Issue Information
روزنامه با شماره پیاپی سال 2011
Pages
4
From page
125
To page
128
Abstract
An improved self-alignment scheme for strapdown Inertial Navigation System (SINS) based on the extended Kalman filter (EKF) and augmented measurements is proposed. Monte Carlo simulations show that the method provides good azimuth alignment, improved rate of convergence of azimuth attitude error and reduction in sensitivity to gyro biases.
Keywords
Measurement augmentation , SINS , Nonlinear filtering , EKF , Self-alignment
Journal title
Aerospace Science and Technology
Serial Year
2011
Journal title
Aerospace Science and Technology
Record number
2230383
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