• 文献检索
  • 文档翻译
  • 深度研究
  • 学术资讯
  • Suppr Zotero 插件Zotero 插件
  • 邀请有礼
  • 套餐&价格
  • 历史记录
应用&插件
Suppr Zotero 插件Zotero 插件浏览器插件Mac 客户端Windows 客户端微信小程序
定价
高级版会员购买积分包购买API积分包
服务
文献检索文档翻译深度研究API 文档MCP 服务
关于我们
关于 Suppr公司介绍联系我们用户协议隐私条款
关注我们

Suppr 超能文献

核心技术专利:CN118964589B侵权必究
粤ICP备2023148730 号-1Suppr @ 2026

文献检索

告别复杂PubMed语法,用中文像聊天一样搜索,搜遍4000万医学文献。AI智能推荐,让科研检索更轻松。

立即免费搜索

文件翻译

保留排版,准确专业,支持PDF/Word/PPT等文件格式,支持 12+语言互译。

免费翻译文档

深度研究

AI帮你快速写综述,25分钟生成高质量综述,智能提取关键信息,辅助科研写作。

立即免费体验

一种基于重力视运动和传感器数据去噪的捷联惯性导航系统自对准算法

A Self-Alignment Algorithm for SINS Based on Gravitational Apparent Motion and Sensor Data Denoising.

作者信息

Liu Yiting, Xu Xiaosu, Liu Xixiang, Yao Yiqing, Wu Liang, Sun Jin

机构信息

Key Laboratory of Micro-Inertial Instrument and Advanced Navigation Technology, Ministry of Education, School of Instrument Science and Engineering, Southeast University, Nanjing 210096, China,.

出版信息

Sensors (Basel). 2015 Apr 27;15(5):9827-53. doi: 10.3390/s150509827.

DOI:10.3390/s150509827
PMID:25923932
原文链接:https://pmc.ncbi.nlm.nih.gov/articles/PMC4481961/
Abstract

Initial alignment is always a key topic and difficult to achieve in an inertial navigation system (INS). In this paper a novel self-initial alignment algorithm is proposed using gravitational apparent motion vectors at three different moments and vector-operation. Simulation and analysis showed that this method easily suffers from the random noise contained in accelerometer measurements which are used to construct apparent motion directly. Aiming to resolve this problem, an online sensor data denoising method based on a Kalman filter is proposed and a novel reconstruction method for apparent motion is designed to avoid the collinearity among vectors participating in the alignment solution. Simulation, turntable tests and vehicle tests indicate that the proposed alignment algorithm can fulfill initial alignment of strapdown INS (SINS) under both static and swinging conditions. The accuracy can either reach or approach the theoretical values determined by sensor precision under static or swinging conditions.

摘要

初始对准始终是惯性导航系统(INS)中的一个关键课题,且难以实现。本文提出了一种利用三个不同时刻的重力视运动矢量和矢量运算的新型自对准算法。仿真与分析表明,该方法容易受到加速度计测量中所含随机噪声的影响,而这些测量数据直接用于构建视运动。为解决这一问题,提出了一种基于卡尔曼滤波器的在线传感器数据去噪方法,并设计了一种新型视运动重构方法,以避免参与对准解算的矢量共线。仿真、转台测试和车辆测试表明,所提出的对准算法能够在静态和摇摆条件下完成捷联惯性导航系统(SINS)的初始对准。在静态或摇摆条件下,精度均可达到或接近由传感器精度确定的理论值。

https://cdn.ncbi.nlm.nih.gov/pmc/blobs/b36a/4481961/4dd790f9c5a6/sensors-15-09827-g012.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/b36a/4481961/abb257f60ecd/sensors-15-09827-g001.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/b36a/4481961/d3068ce5da39/sensors-15-09827-g002.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/b36a/4481961/9d6a02110c36/sensors-15-09827-g003.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/b36a/4481961/4ef99addf459/sensors-15-09827-g004.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/b36a/4481961/8075aebe4b4d/sensors-15-09827-g005.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/b36a/4481961/ba68a819409b/sensors-15-09827-g006.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/b36a/4481961/1c0e0e9a8a1a/sensors-15-09827-g007.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/b36a/4481961/0b50e6a77c15/sensors-15-09827-g008a.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/b36a/4481961/f4e9a23475fa/sensors-15-09827-g009.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/b36a/4481961/39ea61352e23/sensors-15-09827-g010.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/b36a/4481961/8bfea2fc8830/sensors-15-09827-g011.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/b36a/4481961/4dd790f9c5a6/sensors-15-09827-g012.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/b36a/4481961/abb257f60ecd/sensors-15-09827-g001.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/b36a/4481961/d3068ce5da39/sensors-15-09827-g002.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/b36a/4481961/9d6a02110c36/sensors-15-09827-g003.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/b36a/4481961/4ef99addf459/sensors-15-09827-g004.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/b36a/4481961/8075aebe4b4d/sensors-15-09827-g005.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/b36a/4481961/ba68a819409b/sensors-15-09827-g006.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/b36a/4481961/1c0e0e9a8a1a/sensors-15-09827-g007.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/b36a/4481961/0b50e6a77c15/sensors-15-09827-g008a.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/b36a/4481961/f4e9a23475fa/sensors-15-09827-g009.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/b36a/4481961/39ea61352e23/sensors-15-09827-g010.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/b36a/4481961/8bfea2fc8830/sensors-15-09827-g011.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/b36a/4481961/4dd790f9c5a6/sensors-15-09827-g012.jpg

相似文献

1
A Self-Alignment Algorithm for SINS Based on Gravitational Apparent Motion and Sensor Data Denoising.一种基于重力视运动和传感器数据去噪的捷联惯性导航系统自对准算法
Sensors (Basel). 2015 Apr 27;15(5):9827-53. doi: 10.3390/s150509827.
2
An improved self-alignment method for strapdown inertial navigation system based on gravitational apparent motion and dual-vector.一种基于重力视运动和双矢量的捷联惯性导航系统改进自对准方法。
Rev Sci Instrum. 2014 Dec;85(12):125108. doi: 10.1063/1.4903196.
3
A Kalman Filter for SINS Self-Alignment Based on Vector Observation.一种基于矢量观测的捷联惯导系统自对准卡尔曼滤波器。
Sensors (Basel). 2017 Jan 29;17(2):264. doi: 10.3390/s17020264.
4
A Newton iterative optimization combined with window loop calculation algorithm for estimating accelerometer bias based on gravitational apparent motion with excitation of swinging motion.一种基于摆动运动激励下的重力表观运动,结合窗口循环计算算法的牛顿迭代优化方法,用于估计加速度计偏差。
Rev Sci Instrum. 2020 Dec 1;91(12):125102. doi: 10.1063/5.0029584.
5
GAM-Based Mooring Alignment for SINS Based on An Improved CEEMD Denoising Method.基于改进的完备总体平均经验模态分解(CEEMD)去噪方法的捷联惯性导航系统(SINS)的基于广义回归神经网络(GAM)的系泊对准
Sensors (Basel). 2019 Aug 15;19(16):3564. doi: 10.3390/s19163564.
6
A Coarse Alignment Method Based on Digital Filters and Reconstructed Observation Vectors.一种基于数字滤波器和重构观测向量的粗对准方法。
Sensors (Basel). 2017 Mar 29;17(4):709. doi: 10.3390/s17040709.
7
An Optimization-Based Initial Alignment and Calibration Algorithm of Land-Vehicle SINS In-Motion.基于优化的车载捷联惯性导航系统动基座初始对准与标定算法
Sensors (Basel). 2018 Jun 28;18(7):2081. doi: 10.3390/s18072081.
8
An iterative optimization method for estimating accelerometer bias based on gravitational apparent motion with excitation of swinging motion.一种基于摆动运动激励下的重力视运动估计加速度计偏差的迭代优化方法。
Rev Sci Instrum. 2019 Jan;90(1):015102. doi: 10.1063/1.5042442.
9
Application of improved fifth-degree cubature Kalman filter in the nonlinear initial alignment of strapdown inertial navigation system.改进的五阶容积卡尔曼滤波器在捷联惯性导航系统非线性初始对准中的应用
Rev Sci Instrum. 2019 Jan;90(1):015111. doi: 10.1063/1.5061790.
10
An Improved Strapdown Inertial Navigation System Initial Alignment Algorithm for Unmanned Vehicles.一种用于无人机的改进型捷联惯性导航系统初始对准算法。
Sensors (Basel). 2018 Sep 30;18(10):3297. doi: 10.3390/s18103297.

引用本文的文献

1
A SINS/DVL Integrated Positioning System through Filtering Gain Compensation Adaptive Filtering.基于滤波增益补偿自适应滤波的 SINS/DVL 组合定位系统。
Sensors (Basel). 2019 Oct 21;19(20):4576. doi: 10.3390/s19204576.
2
Improved Multistage In-Motion Attitude Determination Alignment Method for Strapdown Inertial Navigation System.捷联惯性导航系统的改进多阶段运动中姿态确定对准方法。
Sensors (Basel). 2019 Oct 21;19(20):4568. doi: 10.3390/s19204568.
3
A Kalman Filter for SINS Self-Alignment Based on Vector Observation.一种基于矢量观测的捷联惯导系统自对准卡尔曼滤波器。

本文引用的文献

1
A robust self-alignment method for ship's strapdown INS under mooring conditions.一种在系泊条件下的船舶捷联惯导自对准鲁棒方法。
Sensors (Basel). 2013 Jun 25;13(7):8103-39. doi: 10.3390/s130708103.
Sensors (Basel). 2017 Jan 29;17(2):264. doi: 10.3390/s17020264.
4
Coarse Alignment of Marine Strapdown INS Based on the Trajectory Fitting of Gravity Movement in the Inertial Space.基于惯性空间重力运动轨迹拟合的船用捷联惯导系统粗对准
Sensors (Basel). 2016 Oct 15;16(10):1714. doi: 10.3390/s16101714.