Three-axis attitude determination with pseudo-bias estimation from gravity/magnetic vector observations

FO Silva, RP Menezes Filho, LA Vieira… - Journal of Guidance …, 2020 - arc.aiaa.org
This paper revisits the stationary alignment problem of attitude and heading reference
systems (AHRSs). The investigation is initiated from the three-axis attitude determination …

A fast strapdown gyrocompassing algorithm based on INS differential errors

MAA Atashgah, H Mohammadkarimi, M Ebrahimi - Scientific Reports, 2023 - nature.com
This paper presents an enhanced algorithm for inertial gyrocompassing using strapdown
sensors, which performs faster than the other available ones. The proposed algorithm is …

Error analysis of accelerometer-and magnetometer-based stationary alignment

FO Silva, LPS Paiva, GS Carvalho - Sensors, 2021 - mdpi.com
This paper revisits the stationary attitude initialization problem, ie, the stationary alignment,
of Attitude and Heading Reference Systems (AHRSs). A detailed and comprehensive error …

Research on IMU Calibration Model Based on Polar Decomposition

G Zhao, M Tan, X Wang, W Liang, S Gao, Z Chen - Micromachines, 2023 - mdpi.com
As an important deterministic error of the inertial measurement unit (IMU), the installation
error has a serious impact on the navigation accuracy of the strapdown inertial navigation …

An Alignment Method Based on KF-ASMUKF Hybrid Filtering for Ship's SINS under Mooring Conditions

P Yao, G Yang, X Peng - Sensors, 2021 - mdpi.com
To solve the problem that the ship's strapdown inertial navigation system (SINS) alignment
accuracy decreases with the increase of the nonlinear filtering state dimension under …

Note on Coarse Alignment of Gyro-Free Inertial Navigation System

H Kim, JH Son, SH Oh, DH Hwang - Sensors, 2023 - mdpi.com
In this note, the feasibility of initial alignment of a gyro-free inertial navigation system (GF-
INS) is investigated. Initial roll and initial pitch are obtained using leveling of conventional …

Non-initial attitude error analysis of SINS by error closed-loop and energy-level constructing

C Tang - Aerospace Science and Technology, 2020 - Elsevier
For the optimization and algorithm design of high precision strapdown inertial navigation
system (SINS), a systematic and fine attitude error analysis method is needed. To this end, a …

Improved multistage in-motion attitude determination alignment method for Strapdown inertial navigation system

H Qiao, M Liu, H Meng, M Wang, W Ke - Sensors, 2019 - mdpi.com
This paper derives an improved multistage in-motion attitude determination alignment
(IMADA) for strapdown inertial navigation system, which integrates the traditional IMADA …

Multi-position calibration method of gyroscopes in inertial measurement unit based on centrifuge with position platform

S Wang, D Chen, N Meng - Microgravity Science and Technology, 2021 - Springer
In order to accurately calibrate the static error model coefficients of three gyroscopes
simultaneously, especially the higher-order coefficients, in an inertial measurement unit, an …