One-Step Initial Alignment Algorithm for SINS in the ECI Frame Based on the Inertial Attitude Measurement of the CNS
To solve the problem of high-precision and fast initial alignment for the Strapdown Inertial Navigation System (SINS) under both dynamic and static conditions, the high-precision attitude measured by the celestial navigation system (CNS) is used as the reference information for the initial alignment...
Main Authors: | Bian, H. (Author), Ma, H. (Author), Tang, J. (Author), Wang, R. (Author) |
---|---|
Format: | Article |
Language: | English |
Published: |
MDPI
2022
|
Subjects: | |
Online Access: | View Fulltext in Publisher |
Similar Items
-
Backtracking Velocity Denoising Based Autonomous In-Motion Initial Alignment
by: Feng Li, et al.
Published: (2018-01-01) -
Initial Alignment of Large Azimuth Misalignment Angles in SINS Based on Adaptive UPF
by: Jin Sun, et al.
Published: (2015-08-01) -
Polar Transversal Initial Alignment Algorithm for UUV with a Large Misalignment Angle
by: Zheping Yan, et al.
Published: (2018-09-01) -
INITIAL ALIGNMENT OF FIBER-OPTIC INERTIAL NAVIGATION SYSTEM WITH LARGE MISALIGNMENT ANGLES BASED ON GENERALIZED PROPORTIONAL-INTEGRAL-DERIVATIVE FILTER
by: Mohammad Ali Rahgoshay, et al.
Published: (2017-09-01) -
In-Motion Attitude and Position Alignment for Odometer-Aided SINS Based on Backtracking Scheme
by: Yiding Sun, et al.
Published: (2019-01-01)