Influence of the Kalman Filtering Initial Setting on SINS Initial Alignment and an Improved Method for the Alignment of Large Misalignment Angles-Reference-Cited by-同舟云学术

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Influence of the Kalman Filtering Initial Setting on SINS Initial Alignment and an Improved Method for the Alignment of Large Misalignment Angles

Published:2023-05-29 Issue: Volume: Page:
ISSN:
Container-title:2023 30th Saint Petersburg International Conference on Integrated Navigation Systems (ICINS)
language:
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Author:

Ning Xiaoge¹,Huang Jixun²,Li Jianxun³

Affiliation:

1. Shanghai Jiao Tong University,School of Electronic Information and Electrical Engineering,Department of Automation,Shanghai,China

2. Beijing Aerospace Times Optical-Electronic Co. Ltd,Beijing,China

3. Beijing Institute of Aerospace Control Devices,Beijing,China

Funder

Research and Development

Publisher

IEEE

Link

http://xplorestaging.ieee.org/ielx7/10168302/10168309/10168421.pdf?arnumber=10168421

Reference9 articles.

1. Initial Alignment by Attitude Estimation for Strapdown Inertial Navigation Systems

2. Pattern Recognition and Machine Learning;bishop;Stat Sci,2006

3. Error Distribution Method and Analysis of Observability Degree Based on the Covariances in Kalman Filter

4. Inertial Navigation Systems with Geodetic Applications;jekeli,2012

5. Principles of GNSS, Inertial, and Multisensor Integrated Navigation Systems;groves,2013

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