• 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

基于互补滤波器的航天飞机捷联惯性导航系统/天文导航系统/全球定位系统组合导航系统信息融合

Information Fusion Based on Complementary Filter for SINS/CNS/GPS Integrated Navigation System of Aerospace Plane.

作者信息

Zhao Yanming, Yan Gongmin, Qin Yongyuan, Fu Qiangwen

机构信息

School of Automation, Northwestern Polytechnical University, Xi'an 710129, China.

出版信息

Sensors (Basel). 2020 Dec 15;20(24):7193. doi: 10.3390/s20247193.

DOI:10.3390/s20247193
PMID:33333963
原文链接:https://pmc.ncbi.nlm.nih.gov/articles/PMC7765422/
Abstract

In order to solve the problems of heavy computational load and poor real time of the information fusion method based on the federated Kalman filter (FKF), a novel information fusion method based on the complementary filter is proposed for strapdown inertial navigation (SINS)/celestial navigation system (CNS)/global positioning system (GPS) integrated navigation system of an aerospace plane. The complementary filters are designed to achieve the estimations of attitude, velocity, and position in the SINS/CNS/GPS integrated navigation system, respectively. The simulation results show that the proposed information fusion method can effectively realize SINS/CNS/GPS information fusion. Compared with FKF, the method based on complementary filter (CF) has the advantages of simplicity, small calculation, good real-time performance, good stability, no need for initial alignment, fast convergence, etc. Furthermore, the computational efficiency of CF is increased by 94.81%. Finally, the superiority of the proposed CF-based method is verified by both the semi-physical simulation and real-time system experiment.

摘要

为了解决基于联邦卡尔曼滤波器(FKF)的信息融合方法计算负荷重、实时性差的问题,针对航天飞机捷联惯性导航系统(SINS)/天文导航系统(CNS)/全球定位系统(GPS)组合导航系统,提出了一种基于互补滤波器的新型信息融合方法。设计互补滤波器分别实现SINS/CNS/GPS组合导航系统中姿态、速度和位置的估计。仿真结果表明,所提出的信息融合方法能够有效实现SINS/CNS/GPS信息融合。与FKF相比,基于互补滤波器(CF)的方法具有简单、计算量小、实时性好、稳定性好、无需初始对准、收敛速度快等优点。此外,CF的计算效率提高了94.81%。最后,通过半物理仿真和实时系统实验验证了所提基于CF方法的优越性。

https://cdn.ncbi.nlm.nih.gov/pmc/blobs/c6c5/7765422/5b32793d4dc2/sensors-20-07193-g017.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/c6c5/7765422/c9caec353720/sensors-20-07193-g001.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/c6c5/7765422/6bcf81fd98ca/sensors-20-07193-g002.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/c6c5/7765422/7711ee3c303c/sensors-20-07193-g003.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/c6c5/7765422/20923a80f5bb/sensors-20-07193-g004.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/c6c5/7765422/3bca0e98d427/sensors-20-07193-g005.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/c6c5/7765422/5fd56454ec13/sensors-20-07193-g006.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/c6c5/7765422/fb7d34a8372a/sensors-20-07193-g007.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/c6c5/7765422/ac0411bb5003/sensors-20-07193-g008.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/c6c5/7765422/fb936a54aca5/sensors-20-07193-g009.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/c6c5/7765422/54963ae15cda/sensors-20-07193-g010.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/c6c5/7765422/e443ab107568/sensors-20-07193-g011.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/c6c5/7765422/15d7a40843d3/sensors-20-07193-g012.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/c6c5/7765422/54401303121f/sensors-20-07193-g013.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/c6c5/7765422/5f057fc18acd/sensors-20-07193-g014.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/c6c5/7765422/98d42f98868c/sensors-20-07193-g015.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/c6c5/7765422/2fd1d4d00eb9/sensors-20-07193-g016.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/c6c5/7765422/5b32793d4dc2/sensors-20-07193-g017.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/c6c5/7765422/c9caec353720/sensors-20-07193-g001.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/c6c5/7765422/6bcf81fd98ca/sensors-20-07193-g002.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/c6c5/7765422/7711ee3c303c/sensors-20-07193-g003.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/c6c5/7765422/20923a80f5bb/sensors-20-07193-g004.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/c6c5/7765422/3bca0e98d427/sensors-20-07193-g005.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/c6c5/7765422/5fd56454ec13/sensors-20-07193-g006.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/c6c5/7765422/fb7d34a8372a/sensors-20-07193-g007.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/c6c5/7765422/ac0411bb5003/sensors-20-07193-g008.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/c6c5/7765422/fb936a54aca5/sensors-20-07193-g009.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/c6c5/7765422/54963ae15cda/sensors-20-07193-g010.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/c6c5/7765422/e443ab107568/sensors-20-07193-g011.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/c6c5/7765422/15d7a40843d3/sensors-20-07193-g012.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/c6c5/7765422/54401303121f/sensors-20-07193-g013.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/c6c5/7765422/5f057fc18acd/sensors-20-07193-g014.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/c6c5/7765422/98d42f98868c/sensors-20-07193-g015.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/c6c5/7765422/2fd1d4d00eb9/sensors-20-07193-g016.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/c6c5/7765422/5b32793d4dc2/sensors-20-07193-g017.jpg

相似文献

1
Information Fusion Based on Complementary Filter for SINS/CNS/GPS Integrated Navigation System of Aerospace Plane.基于互补滤波器的航天飞机捷联惯性导航系统/天文导航系统/全球定位系统组合导航系统信息融合
Sensors (Basel). 2020 Dec 15;20(24):7193. doi: 10.3390/s20247193.
2
A Novel Robust H∞ Filter Based on Krein Space Theory in the SINS/CNS Attitude Reference System.基于Krein空间理论的捷联惯性导航系统/天文导航系统姿态参考系统中的一种新型鲁棒H∞滤波器
Sensors (Basel). 2016 Mar 18;16(3):396. doi: 10.3390/s16030396.
3
SINS/Landmark Integrated Navigation Based on Landmark Attitude Determination.基于地标姿态确定的SINS/地标组合导航
Sensors (Basel). 2019 Jul 1;19(13):2917. doi: 10.3390/s19132917.
4
Maximum Correntropy Unscented Kalman Filter for Ballistic Missile Navigation System based on SINS/CNS Deeply Integrated Mode.基于 SINS/CNS 深度融合模式的弹道导弹导航系统的最大 corrrentropy 无迹卡尔曼滤波。
Sensors (Basel). 2018 May 27;18(6):1724. doi: 10.3390/s18061724.
5
In-Flight Alignment of Integrated SINS/GPS/Polarization/Geomagnetic Navigation System Based on Federal UKF.基于联邦无迹卡尔曼滤波器的集成捷联惯导系统/全球定位系统/极化/地磁导航系统的飞行中对准
Sensors (Basel). 2022 Aug 10;22(16):5985. doi: 10.3390/s22165985.
6
A Fault-Tolerant Polar Grid SINS/DVL/USBL Integrated Navigation Algorithm Based on the Centralized Filter and Relative Position Measurement.基于集中滤波器和相对位置测量的容错极区网格惯导/多普勒计程仪/超短基线组合导航算法
Sensors (Basel). 2019 Sep 10;19(18):3899. doi: 10.3390/s19183899.
7
A Strap-Down Inertial Navigation/Spectrum Red-Shift/Star Sensor (SINS/SRS/SS) Autonomous Integrated System for Spacecraft Navigation.一种用于航天器导航的 strap-down 惯性导航/频谱红移/星敏感器(SINS/SRS/SS)自主集成系统。
Sensors (Basel). 2018 Jun 26;18(7):2039. doi: 10.3390/s18072039.
8
Adaptive Federated IMM Filter for AUV Integrated Navigation Systems.用于自主水下航行器集成导航系统的自适应联邦交互式多模型滤波器
Sensors (Basel). 2020 Nov 28;20(23):6806. doi: 10.3390/s20236806.
9
Application of Adaptive Robust Kalman Filter Base on MCC for SINS/GPS Integrated Navigation.基于MCC的自适应鲁棒卡尔曼滤波器在SINS/GPS组合导航中的应用
Sensors (Basel). 2023 Sep 28;23(19):8131. doi: 10.3390/s23198131.
10
Adaptive H-infinite kalman filter based on multiple fading factors and its application in unmanned underwater vehicle.基于多重衰落因子的自适应H无穷卡尔曼滤波器及其在无人水下航行器中的应用
ISA Trans. 2021 Feb;108:295-304. doi: 10.1016/j.isatra.2020.08.030. Epub 2020 Aug 26.

引用本文的文献

1
In-Flight Alignment of Integrated SINS/GPS/Polarization/Geomagnetic Navigation System Based on Federal UKF.基于联邦无迹卡尔曼滤波器的集成捷联惯导系统/全球定位系统/极化/地磁导航系统的飞行中对准
Sensors (Basel). 2022 Aug 10;22(16):5985. doi: 10.3390/s22165985.

本文引用的文献

1
SINS/CNS/GNSS Integrated Navigation Based on an Improved Federated Sage-Husa Adaptive Filter.基于改进联合Sage-Husa自适应滤波器的SINS/CNS/GNSS组合导航
Sensors (Basel). 2019 Sep 3;19(17):3812. doi: 10.3390/s19173812.
2
Multi-Sensor Optimal Data Fusion Based on the Adaptive Fading Unscented Kalman Filter.基于自适应渐消无迹卡尔曼滤波器的多传感器最优数据融合
Sensors (Basel). 2018 Feb 6;18(2):488. doi: 10.3390/s18020488.