Enhancing Pure Inertial Navigation Accuracy through a Redundant High-Precision Accelerometer-Based Method Utilizing Neural Networks

Author:

He Qinyuan1,Yu Huapeng1ORCID,Liang Dalei1,Yang Xiaozhuo2

Affiliation:

1. National Innovation Institute of Defense Technology, Academy of Military Science, Beijing 100071, China

2. School of Automation Engineering, University of Electronic Science and Technology of China, Chengdu 611731, China

Abstract

The pure inertial navigation system, crucial for autonomous navigation in GPS-denied environments, faces challenges of error accumulation over time, impacting its effectiveness for prolonged missions. Traditional methods to enhance accuracy have focused on improving instrumentation and algorithms but face limitations due to complexity and costs. This study introduces a novel device-level redundant inertial navigation framework using high-precision accelerometers combined with a neural network-based method to refine navigation accuracy. Experimental validation confirms that this integration significantly boosts navigational precision, outperforming conventional system-level redundancy approaches. The proposed method utilizes the advanced capabilities of high-precision accelerometers and deep learning to achieve superior predictive accuracy and error reduction. This research paves the way for the future integration of cutting-edge technologies like high-precision optomechanical and atom interferometer accelerometers, offering new directions for advanced inertial navigation systems and enhancing their application scope in challenging environments.

Publisher

MDPI AG

Reference20 articles.

1. Survey of Model-based Failure Detection and Isolation in Complex Plants;Gertler;IEEE Control Syst. Mag.,1988

2. Tuttle, F.L., Kisslinger, R.L., and Ritzema, D.G. (1990, January 21–25). F-15 S/MTD IFPC Fault Tolerant Design. Proceedings of the IEEE Conference on Aerospace and Electronics, Dayton, OH, USA.

3. Fault Tolerant Digital System Design;Subbarao;Proc. South-Eastcon,1991

4. Evaluating Sensor Orientations for Navigation Performance and Failure Detection;Harrison;IEEE Trans. AES,1977

5. Experimental strapdown redundant s ensor inertial navigation system;Evans;J. Spacecr.,1969

同舟云学术

1.学者识别学者识别

2.学术分析学术分析

3.人才评估人才评估

"同舟云学术"是以全球学者为主线,采集、加工和组织学术论文而形成的新型学术文献查询和分析系统,可以对全球学者进行文献检索和人才价值评估。用户可以通过关注某些学科领域的顶尖人物而持续追踪该领域的学科进展和研究前沿。经过近期的数据扩容,当前同舟云学术共收录了国内外主流学术期刊6万余种,收集的期刊论文及会议论文总量共计约1.5亿篇,并以每天添加12000余篇中外论文的速度递增。我们也可以为用户提供个性化、定制化的学者数据。欢迎来电咨询!咨询电话:010-8811{复制后删除}0370

www.globalauthorid.com

TOP

Copyright © 2019-2024 北京同舟云网络信息技术有限公司
京公网安备11010802033243号  京ICP备18003416号-3