A Technique for Initial Self-Alignment of a Strapdown INS for Space Launch Vehicles-Reference-Cited by-同舟云学术

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A Technique for Initial Self-Alignment of a Strapdown INS for Space Launch Vehicles

Published:2022-05-30 Issue: Volume: Page:
ISSN:
Container-title:2022 29th Saint Petersburg International Conference on Integrated Navigation Systems (ICINS)
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Author:

Vodicheva L.¹,Belsky L.¹,Parysheva Yu.¹

Affiliation:

1. Scientific and Production Association of Automatics,JSC Academician N.A. Semikhatov,Yekaterinburg,Russia

Publisher

IEEE

Link

http://xplorestaging.ieee.org/ielx7/9815262/9815332/09815373.pdf?arnumber=9815373

Reference7 articles.

1. Initial Alignment of a Strapdown Inertial Navigation System on a Stationary Base: Methods and Their Errors;vodicheva;4 St Petersburg International Conference on Integrated Navigation Systems,2013

2. Three-axis attitude determination from vector observations

3. Estimation of Generic Parameters in a Technique for Initial Alignment and Calibration of INS for Space Launch Vehicles

4. Strapdown System Performance Analysis;savage;Advances in Navigation Sensors and Integration Technology,2004

5. Rapid High Precision Initial Alignment and Calibration of Inertial Navigation System of a Flying Vehicle on a Moving Base;belsky;Giroskopiya i Navigatsiya,2001

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. Comparative Analysis of Algorithms for Initial Alignment of a Strapdown INS with the Help of a Gimballed INS;2023 30th Saint Petersburg International Conference on Integrated Navigation Systems (ICINS);2023-05-29

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