2022
DOI: 10.3390/s22207742
|View full text |Cite
|
Sign up to set email alerts
|

Research on the Necessity of Lie Group Strapdown Inertial Integrated Navigation Error Model Based on Euler Angle

Abstract: In response to the lack of specific demonstration and analysis of the research on the necessity of the Lie group strapdown inertial integrated navigation error model based on the Euler angle, two common integrated navigation systems, strapdown inertial navigation system/global navigation satellite system (SINS/GNSS) and strapdown inertial navigation system/doppler velocity log (SINS/DVL), are used as subjects, and the piecewise constant system (PWCS) matrix, based on the Lie group error model, is established. … Show more

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
2

Citation Types

0
2
0

Year Published

2023
2023
2025
2025

Publication Types

Select...
6

Relationship

0
6

Authors

Journals

citations
Cited by 6 publications
(2 citation statements)
references
References 26 publications
0
2
0
Order By: Relevance
“…To alleviate the inconsistency of the coordinate system of the velocity error vector caused by specific force in the traditional process model, Scherzinger proposed a new velocity error transformation, and Wang et al developed the state transformation extended Kalman filter based on this idea [22][23][24]. Recently, the Lie group theory has been introduced in some inertial navigation fields [25][26][27][28][29][30][31][32]. The group of double direct spatial isometries SE 3 (3) is introduced to formulate the attitude matrix, velocity vector, and position vector into a group.…”
Section: Introductionmentioning
confidence: 99%
“…To alleviate the inconsistency of the coordinate system of the velocity error vector caused by specific force in the traditional process model, Scherzinger proposed a new velocity error transformation, and Wang et al developed the state transformation extended Kalman filter based on this idea [22][23][24]. Recently, the Lie group theory has been introduced in some inertial navigation fields [25][26][27][28][29][30][31][32]. The group of double direct spatial isometries SE 3 (3) is introduced to formulate the attitude matrix, velocity vector, and position vector into a group.…”
Section: Introductionmentioning
confidence: 99%
“…Zhu et al derived the quaternion-based error model on the group and compared it to the Euler angle error model and its counterpart on the group [ 14 ]. Qian et al examined the necessity of the Lie group error model from three perspectives: the stability of variance, estimation accuracy, and observability, and proved its superiority to traditional error models [ 15 ].…”
Section: Introductionmentioning
confidence: 99%