A novel method improving the alignment accuracy of a strapdown inertial navigation system on a stationary base

被引:37
作者
Zhang, CB [1 ]
Tian, WF [1 ]
Jin, ZH [1 ]
机构
[1] Shanghai Jiao Tong Univ, Dept Instrumentat Engn, Shanghai 200030, Peoples R China
关键词
SINS; initial alignment; Kalman filtering; state estimation;
D O I
10.1088/0957-0233/15/4/021
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
In the process of initial alignment for a strapdown inertial navigation system (SINS) on a stationary base, the east gyro drift rate is an important factor affecting the alignment accuracy of the azimuth misalignment angle. When the Kalman filtering algorithm is adopted in initial alignment, as the east gyro drift rate cannot be estimated, it yields a constant error in the estimation of the azimuth misalignment angle. In this paper, a novel method is proposed to improve the alignment accuracy. The update equation for the estimate of the east gyro drift rate is established, and the estimation accuracy of the azimuth misalignment angle has been improved greatly through adjusting the estimated value of the east gyro drift rate on the basis of the update equation. Simulation results show that the method proposed in this paper is efficient in initial alignment for a medium accuracy SINS on a stationary base.
引用
收藏
页码:765 / 769
页数:5
相关论文
共 13 条
[1]   CONTROL THEORETIC APPROACH TO INERTIAL NAVIGATION SYSTEMS [J].
BARITZHACK, IY ;
BERMAN, N .
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 1988, 11 (03) :237-245
[2]  
CHENG X, 1997, J EMI
[3]  
De Cecco M, 2003, MEAS SCI TECHNOL, V14, P643, DOI 10.1088/0957-0233/14/5/316
[4]  
DENG Z, 1993, THEORY INERTIAL NAVI
[5]  
Fang JC, 1996, IEEE T AERO ELEC SYS, V32, P1501, DOI 10.1109/7.543871
[6]  
FANG JC, 1998, INITIAL ALIGNMENT IN
[7]  
GOSHENMESKI D, 1997, IEEE T AUTOMAT CONTR, V37, P1225
[8]   UNIFIED APPROACH TO INERTIAL NAVIGATION SYSTEM ERROR MODELING [J].
GOSHENMESKIN, D ;
BARITZHACK, IY .
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 1992, 15 (03) :648-653
[9]  
HAM FM, 1983, IEEE T AERO ELEC SYS, V19, P156
[10]   ERROR ESTIMATION OF INS GROUND ALIGNMENT THROUGH OBSERVABILITY ANALYSIS [J].
JIANG, YF ;
LIN, YP .
IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS, 1992, 28 (01) :92-97