Inertia-radar integrated navigation limited frame measurement variable weight updating method

The invention discloses an inertia-radar integrated navigation limited frame measurement variable weight updating method, which comprises the following steps of: firstly, analyzing and determining a change rule of radar matching positioning accuracy according to ground test and flight test data veri...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Hauptverfasser: ZHAO RUICHAO, TIAN RONGJUN, FAN ZHENHUI, NIU ZHIQI, MIAO HAOCHUN, LU BAOFENG, TAN PENGLI, ZHU QIJU, ZHANG RU, MEI CHUNBO, LI PENG, DING JIANWEI, LIU JUNSHENG, SONG YUHANG, YANG PENGXIANG
Format: Patent
Sprache:chi ; eng
Schlagworte:
Online-Zugang:Volltext bestellen
Tags: Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
container_end_page
container_issue
container_start_page
container_title
container_volume
creator ZHAO RUICHAO
TIAN RONGJUN
FAN ZHENHUI
NIU ZHIQI
MIAO HAOCHUN
LU BAOFENG
TAN PENGLI
ZHU QIJU
ZHANG RU
MEI CHUNBO
LI PENG
DING JIANWEI
LIU JUNSHENG
SONG YUHANG
YANG PENGXIANG
description The invention discloses an inertia-radar integrated navigation limited frame measurement variable weight updating method, which comprises the following steps of: firstly, analyzing and determining a change rule of radar matching positioning accuracy according to ground test and flight test data verification; secondly, according to the change rule, a dynamic measurement weight is designed; and finally, limited frame variable weight weighing is realized in a filter. Compared with the traditional constant value measurement weight, the variable weight measurement updating has the advantages that the utilization of limited frame radar positioning information is more sufficient, the combination precision is higher, and the high-precision inertia-radar combined navigation under the limited frame measurement information can be realized. 本发明公开了一种惯性-雷达组合导航有限帧量测变权重更新方法,首先依据地面测试和飞行试验数据验证,分析确定雷达匹配定位精度的变化规律;其次,依据该变化规律,设计动态量测权重;最后,在滤波器中实现有限帧变权重量测。本发明相较于传统的常值量测权重,变权重量测更新对有限帧雷达定位信息的利用更充分,组合精度更高,能够实现有限帧量测信息下的高精度惯性-雷达组合导航。
format Patent
fullrecord <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_CN117968680A</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>CN117968680A</sourcerecordid><originalsourceid>FETCH-epo_espacenet_CN117968680A3</originalsourceid><addsrcrecordid>eNqNizEKwkAQRdNYiHqH8QABgxC1lKBoY2UrYXR_NgPZTZhM4vWN4AGsHjzemyePa4SacKrsWEmiwSsbHEUexbNJG6mRIF9VKQdQAPeDIiAajazCzwb0hvjaaOjctEQ_RVa3bpnMKm56rH5cJOvz6V5cUnRtib7jFyKsLG5Ztjvk-3y_OW7_aT5kyT0e</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>Inertia-radar integrated navigation limited frame measurement variable weight updating method</title><source>esp@cenet</source><creator>ZHAO RUICHAO ; TIAN RONGJUN ; FAN ZHENHUI ; NIU ZHIQI ; MIAO HAOCHUN ; LU BAOFENG ; TAN PENGLI ; ZHU QIJU ; ZHANG RU ; MEI CHUNBO ; LI PENG ; DING JIANWEI ; LIU JUNSHENG ; SONG YUHANG ; YANG PENGXIANG</creator><creatorcontrib>ZHAO RUICHAO ; TIAN RONGJUN ; FAN ZHENHUI ; NIU ZHIQI ; MIAO HAOCHUN ; LU BAOFENG ; TAN PENGLI ; ZHU QIJU ; ZHANG RU ; MEI CHUNBO ; LI PENG ; DING JIANWEI ; LIU JUNSHENG ; SONG YUHANG ; YANG PENGXIANG</creatorcontrib><description>The invention discloses an inertia-radar integrated navigation limited frame measurement variable weight updating method, which comprises the following steps of: firstly, analyzing and determining a change rule of radar matching positioning accuracy according to ground test and flight test data verification; secondly, according to the change rule, a dynamic measurement weight is designed; and finally, limited frame variable weight weighing is realized in a filter. Compared with the traditional constant value measurement weight, the variable weight measurement updating has the advantages that the utilization of limited frame radar positioning information is more sufficient, the combination precision is higher, and the high-precision inertia-radar combined navigation under the limited frame measurement information can be realized. 本发明公开了一种惯性-雷达组合导航有限帧量测变权重更新方法,首先依据地面测试和飞行试验数据验证,分析确定雷达匹配定位精度的变化规律;其次,依据该变化规律,设计动态量测权重;最后,在滤波器中实现有限帧变权重量测。本发明相较于传统的常值量测权重,变权重量测更新对有限帧雷达定位信息的利用更充分,组合精度更高,能够实现有限帧量测信息下的高精度惯性-雷达组合导航。</description><language>chi ; eng</language><subject>ANALOGOUS ARRANGEMENTS USING OTHER WAVES ; CALCULATING ; COMPUTING ; COUNTING ; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES ; ELECTRIC DIGITAL DATA PROCESSING ; GYROSCOPIC INSTRUMENTS ; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION ORRERADIATION OF RADIO WAVES ; MEASURING ; MEASURING DISTANCES, LEVELS OR BEARINGS ; NAVIGATION ; PHOTOGRAMMETRY OR VIDEOGRAMMETRY ; PHYSICS ; RADIO DIRECTION-FINDING ; RADIO NAVIGATION ; SURVEYING ; TESTING</subject><creationdate>2024</creationdate><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktohtml>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&amp;date=20240503&amp;DB=EPODOC&amp;CC=CN&amp;NR=117968680A$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25542,76289</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&amp;date=20240503&amp;DB=EPODOC&amp;CC=CN&amp;NR=117968680A$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>ZHAO RUICHAO</creatorcontrib><creatorcontrib>TIAN RONGJUN</creatorcontrib><creatorcontrib>FAN ZHENHUI</creatorcontrib><creatorcontrib>NIU ZHIQI</creatorcontrib><creatorcontrib>MIAO HAOCHUN</creatorcontrib><creatorcontrib>LU BAOFENG</creatorcontrib><creatorcontrib>TAN PENGLI</creatorcontrib><creatorcontrib>ZHU QIJU</creatorcontrib><creatorcontrib>ZHANG RU</creatorcontrib><creatorcontrib>MEI CHUNBO</creatorcontrib><creatorcontrib>LI PENG</creatorcontrib><creatorcontrib>DING JIANWEI</creatorcontrib><creatorcontrib>LIU JUNSHENG</creatorcontrib><creatorcontrib>SONG YUHANG</creatorcontrib><creatorcontrib>YANG PENGXIANG</creatorcontrib><title>Inertia-radar integrated navigation limited frame measurement variable weight updating method</title><description>The invention discloses an inertia-radar integrated navigation limited frame measurement variable weight updating method, which comprises the following steps of: firstly, analyzing and determining a change rule of radar matching positioning accuracy according to ground test and flight test data verification; secondly, according to the change rule, a dynamic measurement weight is designed; and finally, limited frame variable weight weighing is realized in a filter. Compared with the traditional constant value measurement weight, the variable weight measurement updating has the advantages that the utilization of limited frame radar positioning information is more sufficient, the combination precision is higher, and the high-precision inertia-radar combined navigation under the limited frame measurement information can be realized. 本发明公开了一种惯性-雷达组合导航有限帧量测变权重更新方法,首先依据地面测试和飞行试验数据验证,分析确定雷达匹配定位精度的变化规律;其次,依据该变化规律,设计动态量测权重;最后,在滤波器中实现有限帧变权重量测。本发明相较于传统的常值量测权重,变权重量测更新对有限帧雷达定位信息的利用更充分,组合精度更高,能够实现有限帧量测信息下的高精度惯性-雷达组合导航。</description><subject>ANALOGOUS ARRANGEMENTS USING OTHER WAVES</subject><subject>CALCULATING</subject><subject>COMPUTING</subject><subject>COUNTING</subject><subject>DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES</subject><subject>ELECTRIC DIGITAL DATA PROCESSING</subject><subject>GYROSCOPIC INSTRUMENTS</subject><subject>LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION ORRERADIATION OF RADIO WAVES</subject><subject>MEASURING</subject><subject>MEASURING DISTANCES, LEVELS OR BEARINGS</subject><subject>NAVIGATION</subject><subject>PHOTOGRAMMETRY OR VIDEOGRAMMETRY</subject><subject>PHYSICS</subject><subject>RADIO DIRECTION-FINDING</subject><subject>RADIO NAVIGATION</subject><subject>SURVEYING</subject><subject>TESTING</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2024</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNqNizEKwkAQRdNYiHqH8QABgxC1lKBoY2UrYXR_NgPZTZhM4vWN4AGsHjzemyePa4SacKrsWEmiwSsbHEUexbNJG6mRIF9VKQdQAPeDIiAajazCzwb0hvjaaOjctEQ_RVa3bpnMKm56rH5cJOvz6V5cUnRtib7jFyKsLG5Ztjvk-3y_OW7_aT5kyT0e</recordid><startdate>20240503</startdate><enddate>20240503</enddate><creator>ZHAO RUICHAO</creator><creator>TIAN RONGJUN</creator><creator>FAN ZHENHUI</creator><creator>NIU ZHIQI</creator><creator>MIAO HAOCHUN</creator><creator>LU BAOFENG</creator><creator>TAN PENGLI</creator><creator>ZHU QIJU</creator><creator>ZHANG RU</creator><creator>MEI CHUNBO</creator><creator>LI PENG</creator><creator>DING JIANWEI</creator><creator>LIU JUNSHENG</creator><creator>SONG YUHANG</creator><creator>YANG PENGXIANG</creator><scope>EVB</scope></search><sort><creationdate>20240503</creationdate><title>Inertia-radar integrated navigation limited frame measurement variable weight updating method</title><author>ZHAO RUICHAO ; TIAN RONGJUN ; FAN ZHENHUI ; NIU ZHIQI ; MIAO HAOCHUN ; LU BAOFENG ; TAN PENGLI ; ZHU QIJU ; ZHANG RU ; MEI CHUNBO ; LI PENG ; DING JIANWEI ; LIU JUNSHENG ; SONG YUHANG ; YANG PENGXIANG</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_CN117968680A3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>chi ; eng</language><creationdate>2024</creationdate><topic>ANALOGOUS ARRANGEMENTS USING OTHER WAVES</topic><topic>CALCULATING</topic><topic>COMPUTING</topic><topic>COUNTING</topic><topic>DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES</topic><topic>ELECTRIC DIGITAL DATA PROCESSING</topic><topic>GYROSCOPIC INSTRUMENTS</topic><topic>LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION ORRERADIATION OF RADIO WAVES</topic><topic>MEASURING</topic><topic>MEASURING DISTANCES, LEVELS OR BEARINGS</topic><topic>NAVIGATION</topic><topic>PHOTOGRAMMETRY OR VIDEOGRAMMETRY</topic><topic>PHYSICS</topic><topic>RADIO DIRECTION-FINDING</topic><topic>RADIO NAVIGATION</topic><topic>SURVEYING</topic><topic>TESTING</topic><toplevel>online_resources</toplevel><creatorcontrib>ZHAO RUICHAO</creatorcontrib><creatorcontrib>TIAN RONGJUN</creatorcontrib><creatorcontrib>FAN ZHENHUI</creatorcontrib><creatorcontrib>NIU ZHIQI</creatorcontrib><creatorcontrib>MIAO HAOCHUN</creatorcontrib><creatorcontrib>LU BAOFENG</creatorcontrib><creatorcontrib>TAN PENGLI</creatorcontrib><creatorcontrib>ZHU QIJU</creatorcontrib><creatorcontrib>ZHANG RU</creatorcontrib><creatorcontrib>MEI CHUNBO</creatorcontrib><creatorcontrib>LI PENG</creatorcontrib><creatorcontrib>DING JIANWEI</creatorcontrib><creatorcontrib>LIU JUNSHENG</creatorcontrib><creatorcontrib>SONG YUHANG</creatorcontrib><creatorcontrib>YANG PENGXIANG</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>ZHAO RUICHAO</au><au>TIAN RONGJUN</au><au>FAN ZHENHUI</au><au>NIU ZHIQI</au><au>MIAO HAOCHUN</au><au>LU BAOFENG</au><au>TAN PENGLI</au><au>ZHU QIJU</au><au>ZHANG RU</au><au>MEI CHUNBO</au><au>LI PENG</au><au>DING JIANWEI</au><au>LIU JUNSHENG</au><au>SONG YUHANG</au><au>YANG PENGXIANG</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Inertia-radar integrated navigation limited frame measurement variable weight updating method</title><date>2024-05-03</date><risdate>2024</risdate><abstract>The invention discloses an inertia-radar integrated navigation limited frame measurement variable weight updating method, which comprises the following steps of: firstly, analyzing and determining a change rule of radar matching positioning accuracy according to ground test and flight test data verification; secondly, according to the change rule, a dynamic measurement weight is designed; and finally, limited frame variable weight weighing is realized in a filter. Compared with the traditional constant value measurement weight, the variable weight measurement updating has the advantages that the utilization of limited frame radar positioning information is more sufficient, the combination precision is higher, and the high-precision inertia-radar combined navigation under the limited frame measurement information can be realized. 本发明公开了一种惯性-雷达组合导航有限帧量测变权重更新方法,首先依据地面测试和飞行试验数据验证,分析确定雷达匹配定位精度的变化规律;其次,依据该变化规律,设计动态量测权重;最后,在滤波器中实现有限帧变权重量测。本发明相较于传统的常值量测权重,变权重量测更新对有限帧雷达定位信息的利用更充分,组合精度更高,能够实现有限帧量测信息下的高精度惯性-雷达组合导航。</abstract><oa>free_for_read</oa></addata></record>
fulltext fulltext_linktorsrc
identifier
ispartof
issn
language chi ; eng
recordid cdi_epo_espacenet_CN117968680A
source esp@cenet
subjects ANALOGOUS ARRANGEMENTS USING OTHER WAVES
CALCULATING
COMPUTING
COUNTING
DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES
ELECTRIC DIGITAL DATA PROCESSING
GYROSCOPIC INSTRUMENTS
LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION ORRERADIATION OF RADIO WAVES
MEASURING
MEASURING DISTANCES, LEVELS OR BEARINGS
NAVIGATION
PHOTOGRAMMETRY OR VIDEOGRAMMETRY
PHYSICS
RADIO DIRECTION-FINDING
RADIO NAVIGATION
SURVEYING
TESTING
title Inertia-radar integrated navigation limited frame measurement variable weight updating method
url https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-02-07T04%3A35%3A25IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-epo_EVB&rft_val_fmt=info:ofi/fmt:kev:mtx:patent&rft.genre=patent&rft.au=ZHAO%20RUICHAO&rft.date=2024-05-03&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3ECN117968680A%3C/epo_EVB%3E%3Curl%3E%3C/url%3E&disable_directlink=true&sfx.directlink=off&sfx.report_link=0&rft_id=info:oai/&rft_id=info:pmid/&rfr_iscdi=true