In-orbit geometric calibration method for linear array swing scanning type optical remote sensing satellite
The invention discloses an in-orbit geometric calibration method for a linear array sweep-type optical remote sensing satellite, and the method comprises the following steps: 1, obtaining a ground control point on a linear array sweep-type optical remote sensing satellite image from high-precision r...
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 | HUANG AOJIONG CAO JINSHAN YE ZHIWEI |
description | The invention discloses an in-orbit geometric calibration method for a linear array sweep-type optical remote sensing satellite, and the method comprises the following steps: 1, obtaining a ground control point on a linear array sweep-type optical remote sensing satellite image from high-precision reference data through an image matching or manual measurement mode; 2, according to the imaging geometrical relationship of the linear array swing-scanning optical satellite, constructing an in-orbit geometric calibration model of the linear array swing-scanning optical satellite; and step 3, solving imaging geometric parameters of the linear array sweep optical satellite by using ground control points and adopting a step-by-step solving strategy. According to the method, accurate solving of the linear array swing-scanning type optical satellite imaging geometric parameters can be realized, so that support is provided for high-precision geometric processing of linear array swing-scanning type optical satellite imag |
format | Patent |
fullrecord | <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_CN115164938A</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>CN115164938A</sourcerecordid><originalsourceid>FETCH-epo_espacenet_CN115164938A3</originalsourceid><addsrcrecordid>eNqNi70KwlAMRrs4iPoO8QE6FH_QUYqii5N7SWtag7fJJTcgfXur-ABO3-Fwvmn2vEiuVrNDR9qTGzfQYODa0FkFRvXQO7RqEFgIDdAMB0gvlg5SgyIf8CESaHQev2DUqxMkkvSN0CkEdppnkxZDosVvZ9nydLyV55yiVpQiNiTkVXktik2xXe9Xu8Pqn-YNJRhCHA</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>In-orbit geometric calibration method for linear array swing scanning type optical remote sensing satellite</title><source>esp@cenet</source><creator>HUANG AOJIONG ; CAO JINSHAN ; YE ZHIWEI</creator><creatorcontrib>HUANG AOJIONG ; CAO JINSHAN ; YE ZHIWEI</creatorcontrib><description>The invention discloses an in-orbit geometric calibration method for a linear array sweep-type optical remote sensing satellite, and the method comprises the following steps: 1, obtaining a ground control point on a linear array sweep-type optical remote sensing satellite image from high-precision reference data through an image matching or manual measurement mode; 2, according to the imaging geometrical relationship of the linear array swing-scanning optical satellite, constructing an in-orbit geometric calibration model of the linear array swing-scanning optical satellite; and step 3, solving imaging geometric parameters of the linear array sweep optical satellite by using ground control points and adopting a step-by-step solving strategy. According to the method, accurate solving of the linear array swing-scanning type optical satellite imaging geometric parameters can be realized, so that support is provided for high-precision geometric processing of linear array swing-scanning type optical satellite imag</description><language>chi ; eng</language><subject>GYROSCOPIC INSTRUMENTS ; MEASURING ; MEASURING DISTANCES, LEVELS OR BEARINGS ; 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&date=20221011&DB=EPODOC&CC=CN&NR=115164938A$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25542,76290</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20221011&DB=EPODOC&CC=CN&NR=115164938A$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>HUANG AOJIONG</creatorcontrib><creatorcontrib>CAO JINSHAN</creatorcontrib><creatorcontrib>YE ZHIWEI</creatorcontrib><title>In-orbit geometric calibration method for linear array swing scanning type optical remote sensing satellite</title><description>The invention discloses an in-orbit geometric calibration method for a linear array sweep-type optical remote sensing satellite, and the method comprises the following steps: 1, obtaining a ground control point on a linear array sweep-type optical remote sensing satellite image from high-precision reference data through an image matching or manual measurement mode; 2, according to the imaging geometrical relationship of the linear array swing-scanning optical satellite, constructing an in-orbit geometric calibration model of the linear array swing-scanning optical satellite; and step 3, solving imaging geometric parameters of the linear array sweep optical satellite by using ground control points and adopting a step-by-step solving strategy. According to the method, accurate solving of the linear array swing-scanning type optical satellite imaging geometric parameters can be realized, so that support is provided for high-precision geometric processing of linear array swing-scanning type optical satellite imag</description><subject>GYROSCOPIC INSTRUMENTS</subject><subject>MEASURING</subject><subject>MEASURING DISTANCES, LEVELS OR BEARINGS</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>eNqNi70KwlAMRrs4iPoO8QE6FH_QUYqii5N7SWtag7fJJTcgfXur-ABO3-Fwvmn2vEiuVrNDR9qTGzfQYODa0FkFRvXQO7RqEFgIDdAMB0gvlg5SgyIf8CESaHQev2DUqxMkkvSN0CkEdppnkxZDosVvZ9nydLyV55yiVpQiNiTkVXktik2xXe9Xu8Pqn-YNJRhCHA</recordid><startdate>20221011</startdate><enddate>20221011</enddate><creator>HUANG AOJIONG</creator><creator>CAO JINSHAN</creator><creator>YE ZHIWEI</creator><scope>EVB</scope></search><sort><creationdate>20221011</creationdate><title>In-orbit geometric calibration method for linear array swing scanning type optical remote sensing satellite</title><author>HUANG AOJIONG ; CAO JINSHAN ; YE ZHIWEI</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_CN115164938A3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>chi ; eng</language><creationdate>2022</creationdate><topic>GYROSCOPIC INSTRUMENTS</topic><topic>MEASURING</topic><topic>MEASURING DISTANCES, LEVELS OR BEARINGS</topic><topic>NAVIGATION</topic><topic>PHOTOGRAMMETRY OR VIDEOGRAMMETRY</topic><topic>PHYSICS</topic><topic>SURVEYING</topic><topic>TESTING</topic><toplevel>online_resources</toplevel><creatorcontrib>HUANG AOJIONG</creatorcontrib><creatorcontrib>CAO JINSHAN</creatorcontrib><creatorcontrib>YE ZHIWEI</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>HUANG AOJIONG</au><au>CAO JINSHAN</au><au>YE ZHIWEI</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>In-orbit geometric calibration method for linear array swing scanning type optical remote sensing satellite</title><date>2022-10-11</date><risdate>2022</risdate><abstract>The invention discloses an in-orbit geometric calibration method for a linear array sweep-type optical remote sensing satellite, and the method comprises the following steps: 1, obtaining a ground control point on a linear array sweep-type optical remote sensing satellite image from high-precision reference data through an image matching or manual measurement mode; 2, according to the imaging geometrical relationship of the linear array swing-scanning optical satellite, constructing an in-orbit geometric calibration model of the linear array swing-scanning optical satellite; and step 3, solving imaging geometric parameters of the linear array sweep optical satellite by using ground control points and adopting a step-by-step solving strategy. According to the method, accurate solving of the linear array swing-scanning type optical satellite imaging geometric parameters can be realized, so that support is provided for high-precision geometric processing of linear array swing-scanning type optical satellite imag</abstract><oa>free_for_read</oa></addata></record> |
fulltext | fulltext_linktorsrc |
identifier | |
ispartof | |
issn | |
language | chi ; eng |
recordid | cdi_epo_espacenet_CN115164938A |
source | esp@cenet |
subjects | GYROSCOPIC INSTRUMENTS MEASURING MEASURING DISTANCES, LEVELS OR BEARINGS NAVIGATION PHOTOGRAMMETRY OR VIDEOGRAMMETRY PHYSICS SURVEYING TESTING |
title | In-orbit geometric calibration method for linear array swing scanning type optical remote sensing satellite |
url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-30T22%3A15%3A30IST&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=HUANG%20AOJIONG&rft.date=2022-10-11&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3ECN115164938A%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 |