A FAST INITIAL ALIGNMENT METHOD FOR STRAPDOWN INERTIAL NAVIGATION SYSTEM ON STATIONARY BASE

Authors
FANG JC WAN DJ
Citation
Jc. Fang et Dj. Wan, A FAST INITIAL ALIGNMENT METHOD FOR STRAPDOWN INERTIAL NAVIGATION SYSTEM ON STATIONARY BASE, IEEE transactions on aerospace and electronic systems, 32(4), 1996, pp. 1501-1505
Citations number
6
Categorie Soggetti
Telecommunications,"Engineering, Eletrical & Electronic","Aerospace Engineering & Tecnology
Journal title
IEEE transactions on aerospace and electronic systems → ACNP
ISSN journal
00189251
Volume
32
Issue
4
Year of publication
1996
Pages
1501 - 1505
Database
ISI
SICI code
0018-9251(1996)32:4<1501:AFIAMF>2.0.ZU;2-6
Abstract
In this paper a strapdown inertial navigation system (SINS) error mode l is introduced, and the observability of the SINS error model is anal yzed Then, on the basis of this SINS error model and the analysis of c omputer simulation results, a fast estimation method of the azimuth er ror Phi(D) is proposed for the initial alignment of SINS on stationary base. Consequently, the time of initial alignment is reduced greatly. The computer simulation results illustrate the efficiency of this fas t initial alignment method.