Initial alignment in the presence of large misalignment angles is a critical issue in strapdown inertial navigation systems. The large initial misalignment angle adversely affects the accuracy and rapidness of the alignment process. In this paper a novel robust alignment approach is proposed based on a generalized proportional-integral-derivative filter. The proposed alignment approach has some significant advantages compared to the standard Kalman filter based alignment method. This method increases the accuracy and the convergence speed of the alignment process in the large misalignment angles problem. Experimental results also, verify the prominent performance of the presented approach in comparison to conventional standard Kalman filter...
A new moving state marine initial alignment method of strap-down inertial navigation system (SINS) i...
Copyright © 2014 Fu-Jun Pei et al. This is an open access article distributed under the Creative Com...
In this paper, GPS aided in-flight alignment algorithm using UKF(Unscented Kalman Filter) is present...
Initial alignment in the presence of large misalignment angles is a critical issue in strapdown iner...
In the initial alignment process of strapdown inertial navigation system (SINS), large initial misal...
When the misalignment angle is a large angle in the strapdown inertial navigation system (SINS), it ...
In view of the fact the accuracy of the third-degree Cubature Kalman Filter (CKF) used for initial a...
The case of large azimuth misalignment angles in a strapdown inertial navigation system (SINS) is an...
In this paper, a new alignment algorithm that uses simultaneously both open-loop and closedloop sch...
Two different coarse alignment algorithms for Fiber Optic Gyro (FOG) Inertial Navigation System (INS...
In this paper, an innovative inertial navigation system (INS) mechanization and the associated Kalma...
Along with the development of computer technology and informatization, the unmanned vehicle has beco...
Iterative algorithms based on saved data have been researched for strapdown inertial navigation syst...
In this paper, GPS aided in-flight alignment algorithm using UKF is presented for an SDINS under lar...
An accurate initial alignment must be required for inertial navigation system (INS). The performance...
A new moving state marine initial alignment method of strap-down inertial navigation system (SINS) i...
Copyright © 2014 Fu-Jun Pei et al. This is an open access article distributed under the Creative Com...
In this paper, GPS aided in-flight alignment algorithm using UKF(Unscented Kalman Filter) is present...
Initial alignment in the presence of large misalignment angles is a critical issue in strapdown iner...
In the initial alignment process of strapdown inertial navigation system (SINS), large initial misal...
When the misalignment angle is a large angle in the strapdown inertial navigation system (SINS), it ...
In view of the fact the accuracy of the third-degree Cubature Kalman Filter (CKF) used for initial a...
The case of large azimuth misalignment angles in a strapdown inertial navigation system (SINS) is an...
In this paper, a new alignment algorithm that uses simultaneously both open-loop and closedloop sch...
Two different coarse alignment algorithms for Fiber Optic Gyro (FOG) Inertial Navigation System (INS...
In this paper, an innovative inertial navigation system (INS) mechanization and the associated Kalma...
Along with the development of computer technology and informatization, the unmanned vehicle has beco...
Iterative algorithms based on saved data have been researched for strapdown inertial navigation syst...
In this paper, GPS aided in-flight alignment algorithm using UKF is presented for an SDINS under lar...
An accurate initial alignment must be required for inertial navigation system (INS). The performance...
A new moving state marine initial alignment method of strap-down inertial navigation system (SINS) i...
Copyright © 2014 Fu-Jun Pei et al. This is an open access article distributed under the Creative Com...
In this paper, GPS aided in-flight alignment algorithm using UKF(Unscented Kalman Filter) is present...