METHOD FORMING SIGNAL CONTROLLING POSITION OF SENSITIVITY AXIS OF GRAVIMETER INSTALLED ABOARD AIRCRAFT WITH ITS REMOTE SETTING BY PLUMB LINE

METHOD FORMING SIGNAL CONTROLLING POSITION OF SENSITIVITY AXIS OF GRAVIMETER INSTALLED ABOARD AIRCRAFT WITH ITS REMOTE SETTING BY PLUMB LINE

FIELD: aviation instrumentation, aerogravimetric operations in which gravimeter is utilized as transmitter of primary information. SUBSTANCE: collection of signals measured with the help of aboard inertial navigation system mounted in aircraft and corresponding to angles of roll, course and pitch, i...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Hauptverfasser: CHESNOKOV G.I, TRUBITSIN G.V, POLJAKOV L.G, KRJUKOV S.P
Format: Patent
Sprache:eng ; rus
Schlagworte:
GYROSCOPIC INSTRUMENTS
MEASURING
MEASURING DISTANCES, LEVELS OR BEARINGS
NAVIGATION
PHOTOGRAMMETRY OR VIDEOGRAMMETRY
PHYSICS
SURVEYING
TESTING
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 CHESNOKOV G.I
TRUBITSIN G.V
POLJAKOV L.G
KRJUKOV S.P
description FIELD: aviation instrumentation, aerogravimetric operations in which gravimeter is utilized as transmitter of primary information. SUBSTANCE: collection of signals measured with the help of aboard inertial navigation system mounted in aircraft and corresponding to angles of roll, course and pitch, increments of speed caused by Coriolis acceleration and curvature radii are employed to form signal corresponding to angular velocity of sensitivity axis of gravimeter. Difference between newly formed signal and signal corresponding to angular velocity of accompanying trihedron computed with the aid of aboard inertial navigation system is established. Signal controlling position of sensitivity axis of gravimeter is formed by signal of closure error of angular velocities of real motion of sensitivity axis of gravimeter and plumb line realized in precision inertial navigation system. EFFECT: increased precision of remote setting of sensitivity axis of gravimeter. 11 dwg
format Patent
fullrecord <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_RU2221990C2</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>RU2221990C2</sourcerecordid><originalsourceid>FETCH-epo_espacenet_RU2221990C23</originalsourceid><addsrcrecordid>eNqNjUEOgjAQRdm4MOod5gImWlcsCxSYpHTIdERZEWLqyigJHsNDWxIP4Ornv_y8v04-jZGaCiiJG3QVeKyctpCTEyZrF9SSR0FyQCV445bSofSgr-gXVrHuMGoMAzov2lpTgM5IcwzknHUpcEGpAcUDm4bERJHIIs96aO25ySBemW2yuo-POex-uUmgNJLX-zC9hjBP4y08w3vgs1LqmKaHXJ3-mHwBKTk_lg</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>METHOD FORMING SIGNAL CONTROLLING POSITION OF SENSITIVITY AXIS OF GRAVIMETER INSTALLED ABOARD AIRCRAFT WITH ITS REMOTE SETTING BY PLUMB LINE</title><source>esp@cenet</source><creator>CHESNOKOV G.I ; TRUBITSIN G.V ; POLJAKOV L.G ; KRJUKOV S.P</creator><creatorcontrib>CHESNOKOV G.I ; TRUBITSIN G.V ; POLJAKOV L.G ; KRJUKOV S.P</creatorcontrib><description>FIELD: aviation instrumentation, aerogravimetric operations in which gravimeter is utilized as transmitter of primary information. SUBSTANCE: collection of signals measured with the help of aboard inertial navigation system mounted in aircraft and corresponding to angles of roll, course and pitch, increments of speed caused by Coriolis acceleration and curvature radii are employed to form signal corresponding to angular velocity of sensitivity axis of gravimeter. Difference between newly formed signal and signal corresponding to angular velocity of accompanying trihedron computed with the aid of aboard inertial navigation system is established. Signal controlling position of sensitivity axis of gravimeter is formed by signal of closure error of angular velocities of real motion of sensitivity axis of gravimeter and plumb line realized in precision inertial navigation system. EFFECT: increased precision of remote setting of sensitivity axis of gravimeter. 11 dwg</description><edition>7</edition><language>eng ; rus</language><subject>GYROSCOPIC INSTRUMENTS ; MEASURING ; MEASURING DISTANCES, LEVELS OR BEARINGS ; NAVIGATION ; PHOTOGRAMMETRY OR VIDEOGRAMMETRY ; PHYSICS ; SURVEYING ; TESTING</subject><creationdate>2004</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=20040120&amp;DB=EPODOC&amp;CC=RU&amp;NR=2221990C2$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,777,882,25545,76296</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&amp;date=20040120&amp;DB=EPODOC&amp;CC=RU&amp;NR=2221990C2$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>CHESNOKOV G.I</creatorcontrib><creatorcontrib>TRUBITSIN G.V</creatorcontrib><creatorcontrib>POLJAKOV L.G</creatorcontrib><creatorcontrib>KRJUKOV S.P</creatorcontrib><title>METHOD FORMING SIGNAL CONTROLLING POSITION OF SENSITIVITY AXIS OF GRAVIMETER INSTALLED ABOARD AIRCRAFT WITH ITS REMOTE SETTING BY PLUMB LINE</title><description>FIELD: aviation instrumentation, aerogravimetric operations in which gravimeter is utilized as transmitter of primary information. SUBSTANCE: collection of signals measured with the help of aboard inertial navigation system mounted in aircraft and corresponding to angles of roll, course and pitch, increments of speed caused by Coriolis acceleration and curvature radii are employed to form signal corresponding to angular velocity of sensitivity axis of gravimeter. Difference between newly formed signal and signal corresponding to angular velocity of accompanying trihedron computed with the aid of aboard inertial navigation system is established. Signal controlling position of sensitivity axis of gravimeter is formed by signal of closure error of angular velocities of real motion of sensitivity axis of gravimeter and plumb line realized in precision inertial navigation system. EFFECT: increased precision of remote setting of sensitivity axis of gravimeter. 11 dwg</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>2004</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNqNjUEOgjAQRdm4MOod5gImWlcsCxSYpHTIdERZEWLqyigJHsNDWxIP4Ornv_y8v04-jZGaCiiJG3QVeKyctpCTEyZrF9SSR0FyQCV445bSofSgr-gXVrHuMGoMAzov2lpTgM5IcwzknHUpcEGpAcUDm4bERJHIIs96aO25ySBemW2yuo-POex-uUmgNJLX-zC9hjBP4y08w3vgs1LqmKaHXJ3-mHwBKTk_lg</recordid><startdate>20040120</startdate><enddate>20040120</enddate><creator>CHESNOKOV G.I</creator><creator>TRUBITSIN G.V</creator><creator>POLJAKOV L.G</creator><creator>KRJUKOV S.P</creator><scope>EVB</scope></search><sort><creationdate>20040120</creationdate><title>METHOD FORMING SIGNAL CONTROLLING POSITION OF SENSITIVITY AXIS OF GRAVIMETER INSTALLED ABOARD AIRCRAFT WITH ITS REMOTE SETTING BY PLUMB LINE</title><author>CHESNOKOV G.I ; TRUBITSIN G.V ; POLJAKOV L.G ; KRJUKOV S.P</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_RU2221990C23</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; rus</language><creationdate>2004</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>CHESNOKOV G.I</creatorcontrib><creatorcontrib>TRUBITSIN G.V</creatorcontrib><creatorcontrib>POLJAKOV L.G</creatorcontrib><creatorcontrib>KRJUKOV S.P</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>CHESNOKOV G.I</au><au>TRUBITSIN G.V</au><au>POLJAKOV L.G</au><au>KRJUKOV S.P</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>METHOD FORMING SIGNAL CONTROLLING POSITION OF SENSITIVITY AXIS OF GRAVIMETER INSTALLED ABOARD AIRCRAFT WITH ITS REMOTE SETTING BY PLUMB LINE</title><date>2004-01-20</date><risdate>2004</risdate><abstract>FIELD: aviation instrumentation, aerogravimetric operations in which gravimeter is utilized as transmitter of primary information. SUBSTANCE: collection of signals measured with the help of aboard inertial navigation system mounted in aircraft and corresponding to angles of roll, course and pitch, increments of speed caused by Coriolis acceleration and curvature radii are employed to form signal corresponding to angular velocity of sensitivity axis of gravimeter. Difference between newly formed signal and signal corresponding to angular velocity of accompanying trihedron computed with the aid of aboard inertial navigation system is established. Signal controlling position of sensitivity axis of gravimeter is formed by signal of closure error of angular velocities of real motion of sensitivity axis of gravimeter and plumb line realized in precision inertial navigation system. EFFECT: increased precision of remote setting of sensitivity axis of gravimeter. 11 dwg</abstract><edition>7</edition><oa>free_for_read</oa></addata></record>
fulltext fulltext_linktorsrc
identifier
ispartof
issn
language eng ; rus
recordid cdi_epo_espacenet_RU2221990C2
source esp@cenet
subjects GYROSCOPIC INSTRUMENTS
MEASURING
MEASURING DISTANCES, LEVELS OR BEARINGS
NAVIGATION
PHOTOGRAMMETRY OR VIDEOGRAMMETRY
PHYSICS
SURVEYING
TESTING
title METHOD FORMING SIGNAL CONTROLLING POSITION OF SENSITIVITY AXIS OF GRAVIMETER INSTALLED ABOARD AIRCRAFT WITH ITS REMOTE SETTING BY PLUMB LINE
url https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-18T02%3A55%3A19IST&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=CHESNOKOV%20G.I&rft.date=2004-01-20&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3ERU2221990C2%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