METHOD AND APPARATUS FOR SENSING SATELLITE ATTITUDE
A method and an apparatus for sensing the posture of a satellite are provided to obtain the posture of the satellite through numerical processing of a visual image. A method of sensing the posture of a satellite includes the steps of photographing an image of the earth using an image photographing p...
Gespeichert in:
Hauptverfasser: | , , , |
---|---|
Format: | Patent |
Sprache: | 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 | JEONG, SEONG KYUN BANG, JUN SIK LEE, SANG UK KIM, JAE HOON |
description | A method and an apparatus for sensing the posture of a satellite are provided to obtain the posture of the satellite through numerical processing of a visual image. A method of sensing the posture of a satellite includes the steps of photographing an image of the earth using an image photographing part(S201), determining whether solar eclipse is generated(S202), filtering strong solar light to transmit the light to a posture signal generating part(S203), allocating a photograph image region to the posture signal generating part(S204), obtaining an earth boundary region(S205), calculating variation of the earth boundary region(S206), determining whether the variation value is normal(S207), converting the calculated variation value into an posture signal(S208), and initializing image information(S209). |
format | Patent |
fullrecord | <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_KR100837216BB1</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>KR100837216BB1</sourcerecordid><originalsourceid>FETCH-epo_espacenet_KR100837216BB13</originalsourceid><addsrcrecordid>eNrjZDD2dQ3x8HdRcPQD4oAAxyDHkNBgBTf_IIVgV79gTz93hWDHEFcfH88QVwXHkBDPkFAXVx4G1rTEnOJUXijNzaDs5hri7KGbWpAfn1pckJicmpdaEu8dZGhgYGFsbmRo5uRkaEycKgBAaCgk</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>METHOD AND APPARATUS FOR SENSING SATELLITE ATTITUDE</title><source>esp@cenet</source><creator>JEONG, SEONG KYUN ; BANG, JUN SIK ; LEE, SANG UK ; KIM, JAE HOON</creator><creatorcontrib>JEONG, SEONG KYUN ; BANG, JUN SIK ; LEE, SANG UK ; KIM, JAE HOON</creatorcontrib><description>A method and an apparatus for sensing the posture of a satellite are provided to obtain the posture of the satellite through numerical processing of a visual image. A method of sensing the posture of a satellite includes the steps of photographing an image of the earth using an image photographing part(S201), determining whether solar eclipse is generated(S202), filtering strong solar light to transmit the light to a posture signal generating part(S203), allocating a photograph image region to the posture signal generating part(S204), obtaining an earth boundary region(S205), calculating variation of the earth boundary region(S206), determining whether the variation value is normal(S207), converting the calculated variation value into an posture signal(S208), and initializing image information(S209).</description><language>eng</language><subject>AIRCRAFT ; AVIATION ; COSMONAUTICS ; PERFORMING OPERATIONS ; TRANSPORTING ; VEHICLES OR EQUIPMENT THEREFOR</subject><creationdate>2008</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=20080611&DB=EPODOC&CC=KR&NR=100837216B1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25542,76289</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20080611&DB=EPODOC&CC=KR&NR=100837216B1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>JEONG, SEONG KYUN</creatorcontrib><creatorcontrib>BANG, JUN SIK</creatorcontrib><creatorcontrib>LEE, SANG UK</creatorcontrib><creatorcontrib>KIM, JAE HOON</creatorcontrib><title>METHOD AND APPARATUS FOR SENSING SATELLITE ATTITUDE</title><description>A method and an apparatus for sensing the posture of a satellite are provided to obtain the posture of the satellite through numerical processing of a visual image. A method of sensing the posture of a satellite includes the steps of photographing an image of the earth using an image photographing part(S201), determining whether solar eclipse is generated(S202), filtering strong solar light to transmit the light to a posture signal generating part(S203), allocating a photograph image region to the posture signal generating part(S204), obtaining an earth boundary region(S205), calculating variation of the earth boundary region(S206), determining whether the variation value is normal(S207), converting the calculated variation value into an posture signal(S208), and initializing image information(S209).</description><subject>AIRCRAFT</subject><subject>AVIATION</subject><subject>COSMONAUTICS</subject><subject>PERFORMING OPERATIONS</subject><subject>TRANSPORTING</subject><subject>VEHICLES OR EQUIPMENT THEREFOR</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2008</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZDD2dQ3x8HdRcPQD4oAAxyDHkNBgBTf_IIVgV79gTz93hWDHEFcfH88QVwXHkBDPkFAXVx4G1rTEnOJUXijNzaDs5hri7KGbWpAfn1pckJicmpdaEu8dZGhgYGFsbmRo5uRkaEycKgBAaCgk</recordid><startdate>20080611</startdate><enddate>20080611</enddate><creator>JEONG, SEONG KYUN</creator><creator>BANG, JUN SIK</creator><creator>LEE, SANG UK</creator><creator>KIM, JAE HOON</creator><scope>EVB</scope></search><sort><creationdate>20080611</creationdate><title>METHOD AND APPARATUS FOR SENSING SATELLITE ATTITUDE</title><author>JEONG, SEONG KYUN ; BANG, JUN SIK ; LEE, SANG UK ; KIM, JAE HOON</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_KR100837216BB13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng</language><creationdate>2008</creationdate><topic>AIRCRAFT</topic><topic>AVIATION</topic><topic>COSMONAUTICS</topic><topic>PERFORMING OPERATIONS</topic><topic>TRANSPORTING</topic><topic>VEHICLES OR EQUIPMENT THEREFOR</topic><toplevel>online_resources</toplevel><creatorcontrib>JEONG, SEONG KYUN</creatorcontrib><creatorcontrib>BANG, JUN SIK</creatorcontrib><creatorcontrib>LEE, SANG UK</creatorcontrib><creatorcontrib>KIM, JAE HOON</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>JEONG, SEONG KYUN</au><au>BANG, JUN SIK</au><au>LEE, SANG UK</au><au>KIM, JAE HOON</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>METHOD AND APPARATUS FOR SENSING SATELLITE ATTITUDE</title><date>2008-06-11</date><risdate>2008</risdate><abstract>A method and an apparatus for sensing the posture of a satellite are provided to obtain the posture of the satellite through numerical processing of a visual image. A method of sensing the posture of a satellite includes the steps of photographing an image of the earth using an image photographing part(S201), determining whether solar eclipse is generated(S202), filtering strong solar light to transmit the light to a posture signal generating part(S203), allocating a photograph image region to the posture signal generating part(S204), obtaining an earth boundary region(S205), calculating variation of the earth boundary region(S206), determining whether the variation value is normal(S207), converting the calculated variation value into an posture signal(S208), and initializing image information(S209).</abstract><oa>free_for_read</oa></addata></record> |
fulltext | fulltext_linktorsrc |
identifier | |
ispartof | |
issn | |
language | eng |
recordid | cdi_epo_espacenet_KR100837216BB1 |
source | esp@cenet |
subjects | AIRCRAFT AVIATION COSMONAUTICS PERFORMING OPERATIONS TRANSPORTING VEHICLES OR EQUIPMENT THEREFOR |
title | METHOD AND APPARATUS FOR SENSING SATELLITE ATTITUDE |
url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-02-06T20%3A14%3A45IST&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=JEONG,%20SEONG%20KYUN&rft.date=2008-06-11&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3EKR100837216BB1%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 |