2003•Journal of Chinese Inertial TechnologyRequires access

A Fast and Precision Initial Alignment Method for Strapdown Inertial Navigation System

Shen Gong-xun

Open publisher page 2 citations

Abstract

Although the tradition muliposition alignment technique made the strapdown inertial navigation system (SINS) having high alignment accuracy, the poor observability of SINS on stationary base, the estimation of the azimuth error will converge very slowly in initial alignment by means of Kalman filter. In this paper, a fast and accuracy estimation method of the multiposition alignment azimuth error is creatively proposed for the initial alignment of SINS on stationary base. On the basis of the fast converge of the leveling error, the azimuth error can be directly calculated. By means of this fast and accuracy initial alignment method, not only the precision of initial alignment is increased, but also the speed of initial alignment is greatly improved. The computer simulation results illustrate the efficiency of this method.

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What this paper is about

Although the tradition muliposition alignment technique made the strapdown inertial navigation system (SINS) having high alignment accuracy, the poor observability of SINS on stationary base, the estimation of the azimuth error will converge very slowly in initial alignment by means of Kalman filter. In this paper, a fast and accuracy estimation method of the multiposition alignment azimuth error is creatively proposed for the initial alignment of SINS on stationary base. On the basis of the fast converge of the leveling error, the azimuth error can be directly calculated. By means of this fast and accuracy initial alignment method, not only the precision of initial alignment is increased, but also the speed of initial alignment is greatly improved. The computer simulation results illustrate the efficiency of this method.

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Available abstract

Although the tradition muliposition alignment technique made the strapdown inertial navigation system (SINS) having high alignment accuracy, the poor observability of SINS on stationary base, the estimation of the azimuth error will converge very slowly in initial alignment by means of Kalman filter. In this paper, a fast and accuracy estimation method of the multiposition alignment azimuth error is creatively proposed for the initial alignment of SINS on stationary base. On the basis of the fast converge of the leveling error, the azimuth error can be directly calculated. By means of this fast and accuracy initial alignment method, not only the precision of initial alignment is increased, but also the speed of initial alignment is greatly improved. The computer simulation results illustrate the efficiency of this method.

Key concepts: Inertial navigation system, Azimuth, Kalman filter, Observability, Computer science, Control theory (sociology), Orientation (vector space), Inertial frame of reference

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