Low-orbit satellite time-frequency synchronization method and system, electronic equipment and storage medium
The invention relates to a low-earth-orbit satellite time-frequency synchronization method and system, electronic equipment and a storage medium, and the method comprises the steps: obtaining the observation data of a navigation satellite based on a reference frequency signal of a low-earth-orbit sa...
Gespeichert in:
Hauptverfasser: | , , |
---|---|
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 | YIN XIANGFEI ZHANG YI AI YANJUN |
description | The invention relates to a low-earth-orbit satellite time-frequency synchronization method and system, electronic equipment and a storage medium, and the method comprises the steps: obtaining the observation data of a navigation satellite based on a reference frequency signal of a low-earth-orbit satellite frequency source; wherein the observation data comprises a pseudo-range observation value and a carrier phase observation value; performing precise point positioning based on the pseudo-range observation value, the carrier phase observation value and precise information injected on the ground to obtain position information of the low-orbit satellite; wherein the precise information comprises precise orbit information and precise clock error information of the navigation satellite; determining reference time based on the position information of the low-orbit satellite, and generating a reference time pulse signal; and regulating and controlling on-satellite time of the ground orbit satellite and a reference |
format | Patent |
fullrecord | <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_CN112817022A</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>CN112817022A</sourcerecordid><originalsourceid>FETCH-epo_espacenet_CN112817022A3</originalsourceid><addsrcrecordid>eNqNy7EKwjAUheEuDqK-Q9wN2DroKkVxECf3EtNTG0jurcktUp_eij6A0xnO90-zcOan5nhzopIReO8ESlyAbiIePcgOKg1k28jkXkYckwqQlmtlqB6vJAgrBQ8rH2LVWLkugOQLhKO5Y2xq14d5NmmMT1j8dpYtj4dredLouELqjAVBqvKS58Uu366LYr_5x7wBFDlDOA</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>Low-orbit satellite time-frequency synchronization method and system, electronic equipment and storage medium</title><source>esp@cenet</source><creator>YIN XIANGFEI ; ZHANG YI ; AI YANJUN</creator><creatorcontrib>YIN XIANGFEI ; ZHANG YI ; AI YANJUN</creatorcontrib><description>The invention relates to a low-earth-orbit satellite time-frequency synchronization method and system, electronic equipment and a storage medium, and the method comprises the steps: obtaining the observation data of a navigation satellite based on a reference frequency signal of a low-earth-orbit satellite frequency source; wherein the observation data comprises a pseudo-range observation value and a carrier phase observation value; performing precise point positioning based on the pseudo-range observation value, the carrier phase observation value and precise information injected on the ground to obtain position information of the low-orbit satellite; wherein the precise information comprises precise orbit information and precise clock error information of the navigation satellite; determining reference time based on the position information of the low-orbit satellite, and generating a reference time pulse signal; and regulating and controlling on-satellite time of the ground orbit satellite and a reference</description><language>chi ; eng</language><subject>ANALOGOUS ARRANGEMENTS USING OTHER WAVES ; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES ; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION ORRERADIATION OF RADIO WAVES ; MEASURING ; PHYSICS ; RADIO DIRECTION-FINDING ; RADIO NAVIGATION ; TESTING</subject><creationdate>2021</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&date=20210518&DB=EPODOC&CC=CN&NR=112817022A$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20210518&DB=EPODOC&CC=CN&NR=112817022A$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>YIN XIANGFEI</creatorcontrib><creatorcontrib>ZHANG YI</creatorcontrib><creatorcontrib>AI YANJUN</creatorcontrib><title>Low-orbit satellite time-frequency synchronization method and system, electronic equipment and storage medium</title><description>The invention relates to a low-earth-orbit satellite time-frequency synchronization method and system, electronic equipment and a storage medium, and the method comprises the steps: obtaining the observation data of a navigation satellite based on a reference frequency signal of a low-earth-orbit satellite frequency source; wherein the observation data comprises a pseudo-range observation value and a carrier phase observation value; performing precise point positioning based on the pseudo-range observation value, the carrier phase observation value and precise information injected on the ground to obtain position information of the low-orbit satellite; wherein the precise information comprises precise orbit information and precise clock error information of the navigation satellite; determining reference time based on the position information of the low-orbit satellite, and generating a reference time pulse signal; and regulating and controlling on-satellite time of the ground orbit satellite and a reference</description><subject>ANALOGOUS ARRANGEMENTS USING OTHER WAVES</subject><subject>DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES</subject><subject>LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION ORRERADIATION OF RADIO WAVES</subject><subject>MEASURING</subject><subject>PHYSICS</subject><subject>RADIO DIRECTION-FINDING</subject><subject>RADIO NAVIGATION</subject><subject>TESTING</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2021</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNqNy7EKwjAUheEuDqK-Q9wN2DroKkVxECf3EtNTG0jurcktUp_eij6A0xnO90-zcOan5nhzopIReO8ESlyAbiIePcgOKg1k28jkXkYckwqQlmtlqB6vJAgrBQ8rH2LVWLkugOQLhKO5Y2xq14d5NmmMT1j8dpYtj4dredLouELqjAVBqvKS58Uu366LYr_5x7wBFDlDOA</recordid><startdate>20210518</startdate><enddate>20210518</enddate><creator>YIN XIANGFEI</creator><creator>ZHANG YI</creator><creator>AI YANJUN</creator><scope>EVB</scope></search><sort><creationdate>20210518</creationdate><title>Low-orbit satellite time-frequency synchronization method and system, electronic equipment and storage medium</title><author>YIN XIANGFEI ; ZHANG YI ; AI YANJUN</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_CN112817022A3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>chi ; eng</language><creationdate>2021</creationdate><topic>ANALOGOUS ARRANGEMENTS USING OTHER WAVES</topic><topic>DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES</topic><topic>LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION ORRERADIATION OF RADIO WAVES</topic><topic>MEASURING</topic><topic>PHYSICS</topic><topic>RADIO DIRECTION-FINDING</topic><topic>RADIO NAVIGATION</topic><topic>TESTING</topic><toplevel>online_resources</toplevel><creatorcontrib>YIN XIANGFEI</creatorcontrib><creatorcontrib>ZHANG YI</creatorcontrib><creatorcontrib>AI YANJUN</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>YIN XIANGFEI</au><au>ZHANG YI</au><au>AI YANJUN</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Low-orbit satellite time-frequency synchronization method and system, electronic equipment and storage medium</title><date>2021-05-18</date><risdate>2021</risdate><abstract>The invention relates to a low-earth-orbit satellite time-frequency synchronization method and system, electronic equipment and a storage medium, and the method comprises the steps: obtaining the observation data of a navigation satellite based on a reference frequency signal of a low-earth-orbit satellite frequency source; wherein the observation data comprises a pseudo-range observation value and a carrier phase observation value; performing precise point positioning based on the pseudo-range observation value, the carrier phase observation value and precise information injected on the ground to obtain position information of the low-orbit satellite; wherein the precise information comprises precise orbit information and precise clock error information of the navigation satellite; determining reference time based on the position information of the low-orbit satellite, and generating a reference time pulse signal; and regulating and controlling on-satellite time of the ground orbit satellite and a reference</abstract><oa>free_for_read</oa></addata></record> |
fulltext | fulltext_linktorsrc |
identifier | |
ispartof | |
issn | |
language | chi ; eng |
recordid | cdi_epo_espacenet_CN112817022A |
source | esp@cenet |
subjects | ANALOGOUS ARRANGEMENTS USING OTHER WAVES DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION ORRERADIATION OF RADIO WAVES MEASURING PHYSICS RADIO DIRECTION-FINDING RADIO NAVIGATION TESTING |
title | Low-orbit satellite time-frequency synchronization method and system, electronic equipment and storage medium |
url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2024-12-29T13%3A56%3A39IST&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=YIN%20XIANGFEI&rft.date=2021-05-18&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3ECN112817022A%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 |