Self-Calibration Method for the Errors of Dual-Axis Turntable in Redundant Rotational Inertial Navigation System-Reference-Cited by-同舟云学术

Self-Calibration Method for the Errors of Dual-Axis Turntable in Redundant Rotational Inertial Navigation System

Published:2023-02-01 Issue:3 Volume:23 Page:2411-2421
ISSN:1530-437X
Container-title:IEEE Sensors Journal
language:
Short-container-title:IEEE Sensors J.

Author:

Zhu Ting¹^ORCID,Ren Yuan²^ORCID,Wang Lifen³,Zou Tao³,Chen Yu⁴

Affiliation:

1. School of Automation, Guangxi University of Science and Technology, Liuzhou, China

2. Department of Basic Course, Space Engineering University, Beijing, China

3. Department of Aerospace Science and Technology, Space Engineering University, Beijing, China

4. Beijing Institute of Space Launch Technology, Beijing, China

Funder

National Natural Science Foundation of China

Science and Technology Innovation Cultivation Foundation of Space Engineering University: Moving-Based Alignment Technology of Rocket-Borne Inertial Navigation System in Emergency Launching

Publisher

Institute of Electrical and Electronics Engineers (IEEE)

Subject

Electrical and Electronic Engineering,Instrumentation

Link

http://xplorestaging.ieee.org/ielx7/7361/10032973/09953970.pdf?arnumber=9953970

Reference25 articles.

1. A calibration method of non-orthogonal redundant ring laser gyro inertial navigation system;gao;Proc SPIE,2017

2. An enhanced multi-position calibration method for consumer-grade inertial measurement units applied and tested

3. Analysis and calibration of the mounting errors between inertial measurement unit and turntable in dual-axis rotational inertial navigation system

4. Accurate Compensation of Attitude Angle Error in a Dual-Axis Rotation Inertial Navigation System

5. Improved multi-position calibration for inertial measurement units

Cited by 1 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. A Disturbance Compensation Control Strategy for Rotational Speed Standard Device Based on AMB System;Sensors;2024-05-13