This paper presents a new method for rapid transfer alignment of strapdown inertial navigation system (SINS) by combining the local observability concept with robust adaptive filtering. The system state and observation models are simplified to analyze the observability of the SINS attitude error. Based on the simplified models, the observability matrix and its condition number are constructed to determine the observability degree of SINS during the process of rapid transfer alignment. On the basis of the local obsersability analysis, a robust adaptive filter is developed to estimate the attitude angle error for SINS rapid transfer alignment. Simulation experiments and comparison analysis have been conducted, demonstrating that the proposed ...
In this paper, we proposed a coarse-alignment method for strapdown inertial navigation systems based...
In this paper, a self-alignment method for strapdown inertial navigation systems based on the q-meth...
In the strap-down inertial navigation system (SINS), the initial attitude matrix is acquired through...
Two viewpoints are given: (1) initial alignment of strapdown inertial navigation system (SINS) can b...
Iterative algorithms based on saved data have been researched for strapdown inertial navigation syst...
Copyright © 2014 Fu-Jun Pei et al. This is an open access article distributed under the Creative Com...
Transfer alignment is always a key technology in a strapdown inertial navigation system (SINS) becau...
When the misalignment angle is a large angle in the strapdown inertial navigation system (SINS), it ...
In this paper, an innovative inertial navigation system (INS) mechanization and the associated Kalma...
In the initial alignment process of strapdown inertial navigation system (SINS), large initial misal...
The errors of inertial sensors affect the navigation accuracy of the strapdown inertial navigation s...
Along with the development of computer technology and informatization, the unmanned vehicle has beco...
The case of large azimuth misalignment angles in a strapdown inertial navigation system (SINS) is an...
For a running freely land-vehicle strapdown inertial navigation system (SINS), the problems of self-...
Strapdown inertial navigation system/celestial navigation system (SINS/CNS) integrated navigation is...
In this paper, we proposed a coarse-alignment method for strapdown inertial navigation systems based...
In this paper, a self-alignment method for strapdown inertial navigation systems based on the q-meth...
In the strap-down inertial navigation system (SINS), the initial attitude matrix is acquired through...
Two viewpoints are given: (1) initial alignment of strapdown inertial navigation system (SINS) can b...
Iterative algorithms based on saved data have been researched for strapdown inertial navigation syst...
Copyright © 2014 Fu-Jun Pei et al. This is an open access article distributed under the Creative Com...
Transfer alignment is always a key technology in a strapdown inertial navigation system (SINS) becau...
When the misalignment angle is a large angle in the strapdown inertial navigation system (SINS), it ...
In this paper, an innovative inertial navigation system (INS) mechanization and the associated Kalma...
In the initial alignment process of strapdown inertial navigation system (SINS), large initial misal...
The errors of inertial sensors affect the navigation accuracy of the strapdown inertial navigation s...
Along with the development of computer technology and informatization, the unmanned vehicle has beco...
The case of large azimuth misalignment angles in a strapdown inertial navigation system (SINS) is an...
For a running freely land-vehicle strapdown inertial navigation system (SINS), the problems of self-...
Strapdown inertial navigation system/celestial navigation system (SINS/CNS) integrated navigation is...
In this paper, we proposed a coarse-alignment method for strapdown inertial navigation systems based...
In this paper, a self-alignment method for strapdown inertial navigation systems based on the q-meth...
In the strap-down inertial navigation system (SINS), the initial attitude matrix is acquired through...