In-Motion Initial Alignment Method Based on Vector Observation and Truncated Vectorized <i>K</i>-Matrix for SINS-Reference-Cited by-同舟云学术

In-Motion Initial Alignment Method Based on Vector Observation and Truncated Vectorized K-Matrix for SINS

Published:2022 Issue: Volume:71 Page:1-15
ISSN:0018-9456
Container-title:IEEE Transactions on Instrumentation and Measurement
language:
Short-container-title:IEEE Trans. Instrum. Meas.

Author:

Huang Haoqian¹^ORCID,Wei Jiaying¹^ORCID,Wang Di²^ORCID,Zhang Li³^ORCID,Wang Bing¹^ORCID

Affiliation:

1. College of Energy and Electrical Engineering, Hohai University, Nanjing, China

2. Key Laboratory of Micro-Inertial Instrument and Advanced Navigation Technology, Ministry of Education, School of Instrument Science and Engineering, Southeast University, Nanjing, China

3. Department of Computer Science, Royal Holloway, University of London, Egham, Surrey, U.K.

Funder

Natural Science Foundation of Jiangsu Province

National Natural Science Foundation of China

Fujian Provincial Key Laboratory of Coast and Island Management Technology Study

London Tech Bridge

APEX Undersea Challenge

European Regional Development Fund—Industrial Intensive Innovation Program

Research Fund from the Science and Technology on Underwater Vehicle Technology Laboratory

Water Science and Technology Project of Jiangsu Province

Publisher

Institute of Electrical and Electronics Engineers (IEEE)

Subject

Electrical and Electronic Engineering,Instrumentation

Link

http://xplorestaging.ieee.org/ielx7/19/9717300/09849511.pdf?arnumber=9849511

Reference33 articles.

1. Revisited position-velocity integration formulas for in-flight self-alignment of GPS-aided inertial navigation systems;koja;Proc Brazilian Conf Dyn,2017

2. Optimization-based alignment for strapdown inertial navigation system: comparison and extension

3. A New Fast In-Motion Coarse Alignment Method for GPS-Aided Low-Cost SINS

4. A High-Accuracy GPS-Aided Coarse Alignment Method for MEMS-Based SINS

5. A Quasi-Newton Quaternions Calibration Method for DVL Error Aided GNSS

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