Dynamic calibration system and method for inertial orbit measurement instrument and application of dynamic calibration system and method

The invention discloses a dynamic calibration system and method for an inertial orbit measurement instrument and application of the dynamic calibration system, and the dynamic calibration system is based on the combination of a double-speed sensor and a vehicle-mounted antenna array, and comprises a...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Hauptverfasser: WANG YINGJIE, ZHANG YE, YANG CHAO, SHENG SHIYONG, OUYANG ZIBO, ZHENG HAO, ZHU XINGYONG, WU XISHUI, YANG LIGUANG, WANG XIAOKAI, YAO JIANPING, HE XIAOWEN, LI YUHONG, YE XIAOYU, XIE JIAO, LOU LIANGWEI, HE FUSHOU, LING YONGCHUN, CHEN YUNFENG, SHI JIN, WEI SHAOWEI, CAI DEGOU
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 WANG YINGJIE
ZHANG YE
YANG CHAO
SHENG SHIYONG
OUYANG ZIBO
ZHENG HAO
ZHU XINGYONG
WU XISHUI
YANG LIGUANG
WANG XIAOKAI
YAO JIANPING
HE XIAOWEN
LI YUHONG
YE XIAOYU
XIE JIAO
LOU LIANGWEI
HE FUSHOU
LING YONGCHUN
CHEN YUNFENG
SHI JIN
WEI SHAOWEI
CAI DEGOU
description The invention discloses a dynamic calibration system and method for an inertial orbit measurement instrument and application of the dynamic calibration system, and the dynamic calibration system is based on the combination of a double-speed sensor and a vehicle-mounted antenna array, and comprises a track, a track gauge sensor, an inertial sensor and a differential base station, the center position of each ground antenna of the vehicle-mounted antenna array is provided with a corresponding engineering coordinate system coordinate; the data of the same ground antenna and the data of at least two differential base stations are solved; the track adopts a speed sensor for speed measurement and is matched with a track gauge sensor for course angle deviation measurement; the speed change and the angle change are used for acceleration and angular speed calibration of the inertial sensor; and the differential base station realizes wireless communication with the vehicle-mounted antenna array through a wireless commun
format Patent
fullrecord <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_CN114353835A</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>CN114353835A</sourcerecordid><originalsourceid>FETCH-epo_espacenet_CN114353835A3</originalsourceid><addsrcrecordid>eNqNjTkOwjAQRdNQIOAOwwEoIhOJFiUgKir6aGKPxUjeZE-K3IBjE5YDpPpfen9ZV69uCuhZg0bHQ0bhGKBMRcgDBgOe5BkN2JiBA2VhdBDzwDITLGMmT0FmVCSPX_spYUqO9W8rWjBLLrbVyqIrtPvrptpfL4_2dqAUeyoJNQWSvr3X9VE16qSas1qSeQN8QU1X</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>Dynamic calibration system and method for inertial orbit measurement instrument and application of dynamic calibration system and method</title><source>esp@cenet</source><creator>WANG YINGJIE ; ZHANG YE ; YANG CHAO ; SHENG SHIYONG ; OUYANG ZIBO ; ZHENG HAO ; ZHU XINGYONG ; WU XISHUI ; YANG LIGUANG ; WANG XIAOKAI ; YAO JIANPING ; HE XIAOWEN ; LI YUHONG ; YE XIAOYU ; XIE JIAO ; LOU LIANGWEI ; HE FUSHOU ; LING YONGCHUN ; CHEN YUNFENG ; SHI JIN ; WEI SHAOWEI ; CAI DEGOU</creator><creatorcontrib>WANG YINGJIE ; ZHANG YE ; YANG CHAO ; SHENG SHIYONG ; OUYANG ZIBO ; ZHENG HAO ; ZHU XINGYONG ; WU XISHUI ; YANG LIGUANG ; WANG XIAOKAI ; YAO JIANPING ; HE XIAOWEN ; LI YUHONG ; YE XIAOYU ; XIE JIAO ; LOU LIANGWEI ; HE FUSHOU ; LING YONGCHUN ; CHEN YUNFENG ; SHI JIN ; WEI SHAOWEI ; CAI DEGOU</creatorcontrib><description>The invention discloses a dynamic calibration system and method for an inertial orbit measurement instrument and application of the dynamic calibration system, and the dynamic calibration system is based on the combination of a double-speed sensor and a vehicle-mounted antenna array, and comprises a track, a track gauge sensor, an inertial sensor and a differential base station, the center position of each ground antenna of the vehicle-mounted antenna array is provided with a corresponding engineering coordinate system coordinate; the data of the same ground antenna and the data of at least two differential base stations are solved; the track adopts a speed sensor for speed measurement and is matched with a track gauge sensor for course angle deviation measurement; the speed change and the angle change are used for acceleration and angular speed calibration of the inertial sensor; and the differential base station realizes wireless communication with the vehicle-mounted antenna array through a wireless commun</description><language>chi ; eng</language><subject>GYROSCOPIC INSTRUMENTS ; INDICATING PRESENCE, ABSENCE, OR DIRECTION, OF MOVEMENT ; MEASURING ; MEASURING DISTANCES, LEVELS OR BEARINGS ; MEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION,OR SHOCK ; NAVIGATION ; PHOTOGRAMMETRY OR VIDEOGRAMMETRY ; PHYSICS ; SURVEYING ; TESTING</subject><creationdate>2022</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=20220415&amp;DB=EPODOC&amp;CC=CN&amp;NR=114353835A$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25542,76289</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&amp;date=20220415&amp;DB=EPODOC&amp;CC=CN&amp;NR=114353835A$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>WANG YINGJIE</creatorcontrib><creatorcontrib>ZHANG YE</creatorcontrib><creatorcontrib>YANG CHAO</creatorcontrib><creatorcontrib>SHENG SHIYONG</creatorcontrib><creatorcontrib>OUYANG ZIBO</creatorcontrib><creatorcontrib>ZHENG HAO</creatorcontrib><creatorcontrib>ZHU XINGYONG</creatorcontrib><creatorcontrib>WU XISHUI</creatorcontrib><creatorcontrib>YANG LIGUANG</creatorcontrib><creatorcontrib>WANG XIAOKAI</creatorcontrib><creatorcontrib>YAO JIANPING</creatorcontrib><creatorcontrib>HE XIAOWEN</creatorcontrib><creatorcontrib>LI YUHONG</creatorcontrib><creatorcontrib>YE XIAOYU</creatorcontrib><creatorcontrib>XIE JIAO</creatorcontrib><creatorcontrib>LOU LIANGWEI</creatorcontrib><creatorcontrib>HE FUSHOU</creatorcontrib><creatorcontrib>LING YONGCHUN</creatorcontrib><creatorcontrib>CHEN YUNFENG</creatorcontrib><creatorcontrib>SHI JIN</creatorcontrib><creatorcontrib>WEI SHAOWEI</creatorcontrib><creatorcontrib>CAI DEGOU</creatorcontrib><title>Dynamic calibration system and method for inertial orbit measurement instrument and application of dynamic calibration system and method</title><description>The invention discloses a dynamic calibration system and method for an inertial orbit measurement instrument and application of the dynamic calibration system, and the dynamic calibration system is based on the combination of a double-speed sensor and a vehicle-mounted antenna array, and comprises a track, a track gauge sensor, an inertial sensor and a differential base station, the center position of each ground antenna of the vehicle-mounted antenna array is provided with a corresponding engineering coordinate system coordinate; the data of the same ground antenna and the data of at least two differential base stations are solved; the track adopts a speed sensor for speed measurement and is matched with a track gauge sensor for course angle deviation measurement; the speed change and the angle change are used for acceleration and angular speed calibration of the inertial sensor; and the differential base station realizes wireless communication with the vehicle-mounted antenna array through a wireless commun</description><subject>GYROSCOPIC INSTRUMENTS</subject><subject>INDICATING PRESENCE, ABSENCE, OR DIRECTION, OF MOVEMENT</subject><subject>MEASURING</subject><subject>MEASURING DISTANCES, LEVELS OR BEARINGS</subject><subject>MEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION,OR SHOCK</subject><subject>NAVIGATION</subject><subject>PHOTOGRAMMETRY OR VIDEOGRAMMETRY</subject><subject>PHYSICS</subject><subject>SURVEYING</subject><subject>TESTING</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2022</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNqNjTkOwjAQRdNQIOAOwwEoIhOJFiUgKir6aGKPxUjeZE-K3IBjE5YDpPpfen9ZV69uCuhZg0bHQ0bhGKBMRcgDBgOe5BkN2JiBA2VhdBDzwDITLGMmT0FmVCSPX_spYUqO9W8rWjBLLrbVyqIrtPvrptpfL4_2dqAUeyoJNQWSvr3X9VE16qSas1qSeQN8QU1X</recordid><startdate>20220415</startdate><enddate>20220415</enddate><creator>WANG YINGJIE</creator><creator>ZHANG YE</creator><creator>YANG CHAO</creator><creator>SHENG SHIYONG</creator><creator>OUYANG ZIBO</creator><creator>ZHENG HAO</creator><creator>ZHU XINGYONG</creator><creator>WU XISHUI</creator><creator>YANG LIGUANG</creator><creator>WANG XIAOKAI</creator><creator>YAO JIANPING</creator><creator>HE XIAOWEN</creator><creator>LI YUHONG</creator><creator>YE XIAOYU</creator><creator>XIE JIAO</creator><creator>LOU LIANGWEI</creator><creator>HE FUSHOU</creator><creator>LING YONGCHUN</creator><creator>CHEN YUNFENG</creator><creator>SHI JIN</creator><creator>WEI SHAOWEI</creator><creator>CAI DEGOU</creator><scope>EVB</scope></search><sort><creationdate>20220415</creationdate><title>Dynamic calibration system and method for inertial orbit measurement instrument and application of dynamic calibration system and method</title><author>WANG YINGJIE ; ZHANG YE ; YANG CHAO ; SHENG SHIYONG ; OUYANG ZIBO ; ZHENG HAO ; ZHU XINGYONG ; WU XISHUI ; YANG LIGUANG ; WANG XIAOKAI ; YAO JIANPING ; HE XIAOWEN ; LI YUHONG ; YE XIAOYU ; XIE JIAO ; LOU LIANGWEI ; HE FUSHOU ; LING YONGCHUN ; CHEN YUNFENG ; SHI JIN ; WEI SHAOWEI ; CAI DEGOU</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_CN114353835A3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>chi ; eng</language><creationdate>2022</creationdate><topic>GYROSCOPIC INSTRUMENTS</topic><topic>INDICATING PRESENCE, ABSENCE, OR DIRECTION, OF MOVEMENT</topic><topic>MEASURING</topic><topic>MEASURING DISTANCES, LEVELS OR BEARINGS</topic><topic>MEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION,OR SHOCK</topic><topic>NAVIGATION</topic><topic>PHOTOGRAMMETRY OR VIDEOGRAMMETRY</topic><topic>PHYSICS</topic><topic>SURVEYING</topic><topic>TESTING</topic><toplevel>online_resources</toplevel><creatorcontrib>WANG YINGJIE</creatorcontrib><creatorcontrib>ZHANG YE</creatorcontrib><creatorcontrib>YANG CHAO</creatorcontrib><creatorcontrib>SHENG SHIYONG</creatorcontrib><creatorcontrib>OUYANG ZIBO</creatorcontrib><creatorcontrib>ZHENG HAO</creatorcontrib><creatorcontrib>ZHU XINGYONG</creatorcontrib><creatorcontrib>WU XISHUI</creatorcontrib><creatorcontrib>YANG LIGUANG</creatorcontrib><creatorcontrib>WANG XIAOKAI</creatorcontrib><creatorcontrib>YAO JIANPING</creatorcontrib><creatorcontrib>HE XIAOWEN</creatorcontrib><creatorcontrib>LI YUHONG</creatorcontrib><creatorcontrib>YE XIAOYU</creatorcontrib><creatorcontrib>XIE JIAO</creatorcontrib><creatorcontrib>LOU LIANGWEI</creatorcontrib><creatorcontrib>HE FUSHOU</creatorcontrib><creatorcontrib>LING YONGCHUN</creatorcontrib><creatorcontrib>CHEN YUNFENG</creatorcontrib><creatorcontrib>SHI JIN</creatorcontrib><creatorcontrib>WEI SHAOWEI</creatorcontrib><creatorcontrib>CAI DEGOU</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>WANG YINGJIE</au><au>ZHANG YE</au><au>YANG CHAO</au><au>SHENG SHIYONG</au><au>OUYANG ZIBO</au><au>ZHENG HAO</au><au>ZHU XINGYONG</au><au>WU XISHUI</au><au>YANG LIGUANG</au><au>WANG XIAOKAI</au><au>YAO JIANPING</au><au>HE XIAOWEN</au><au>LI YUHONG</au><au>YE XIAOYU</au><au>XIE JIAO</au><au>LOU LIANGWEI</au><au>HE FUSHOU</au><au>LING YONGCHUN</au><au>CHEN YUNFENG</au><au>SHI JIN</au><au>WEI SHAOWEI</au><au>CAI DEGOU</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Dynamic calibration system and method for inertial orbit measurement instrument and application of dynamic calibration system and method</title><date>2022-04-15</date><risdate>2022</risdate><abstract>The invention discloses a dynamic calibration system and method for an inertial orbit measurement instrument and application of the dynamic calibration system, and the dynamic calibration system is based on the combination of a double-speed sensor and a vehicle-mounted antenna array, and comprises a track, a track gauge sensor, an inertial sensor and a differential base station, the center position of each ground antenna of the vehicle-mounted antenna array is provided with a corresponding engineering coordinate system coordinate; the data of the same ground antenna and the data of at least two differential base stations are solved; the track adopts a speed sensor for speed measurement and is matched with a track gauge sensor for course angle deviation measurement; the speed change and the angle change are used for acceleration and angular speed calibration of the inertial sensor; and the differential base station realizes wireless communication with the vehicle-mounted antenna array through a wireless commun</abstract><oa>free_for_read</oa></addata></record>
fulltext fulltext_linktorsrc
identifier
ispartof
issn
language chi ; eng
recordid cdi_epo_espacenet_CN114353835A
source esp@cenet
subjects GYROSCOPIC INSTRUMENTS
INDICATING PRESENCE, ABSENCE, OR DIRECTION, OF MOVEMENT
MEASURING
MEASURING DISTANCES, LEVELS OR BEARINGS
MEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION,OR SHOCK
NAVIGATION
PHOTOGRAMMETRY OR VIDEOGRAMMETRY
PHYSICS
SURVEYING
TESTING
title Dynamic calibration system and method for inertial orbit measurement instrument and application of dynamic calibration system and method
url https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-02-11T11%3A52%3A59IST&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=WANG%20YINGJIE&rft.date=2022-04-15&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3ECN114353835A%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