OPTICAL-ELECTRONIC SEARCH AND TRACKING SYSTEM
FIELD: transportation, physics. ^ SUBSTANCE: invention relates to defence of aircraft planes (AP) for jamming by infrared target-seeking devices of attacking missles (ITSD). System contains head mirror, movable along two mutually perpendicular axes and provided with aspect sensors, infrared (IR) dir...
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| creator | KHISAMOV RAMIS SHARAFOVICH BELOZEROV AL'BERT FEDOROVICH DOBRYNIN ALEKSANDR ALEKSANDROVICH PRIKHOD'KO VIKTOR NIKITOVICH IVANOV VLADIMIR PETROVICH SUNTSOV VLADIMIR VJACHESLAVOVICH BALOEV VILLEN ARNOL'DOVICH JATSYK VLADIMIR SAMUILOVICH ALEKSEEV JURIJ VITAL'EVICH VAKHITOV MURAT AKHMETOVICH DOROFEEVA MARGARITA VASIL'EVNA |
| description | FIELD: transportation, physics. ^ SUBSTANCE: invention relates to defence of aircraft planes (AP) for jamming by infrared target-seeking devices of attacking missles (ITSD). System contains head mirror, movable along two mutually perpendicular axes and provided with aspect sensors, infrared (IR) direction-finding channel containing lens and photodetector (FD). Between the head mirror and lens at an angle to optical axis fixed flat mirror with axial hole is installed. The hole is positioned at laser emission path from transmitting laser channel. FD output and outputs of head mirror aspect sensors are connected to control-computing unit, control outputs of which are connected to head mirror actuators and to control input of transmitting laser channel. Lens is made of two components between which, in focal plane of the first on emission path component, aperture is installed which prevents diffused laser emission from getting on FD array. At the same time, IR direction-finding channel is receiving laser channel of the system. Determination of error angle between system optical axis and laser signal reflected by target in IR direction-finding channel provides improvement of accuracy of laser emission pointing at ITSD of attacking missiles. Angular-rate sensors installed on head mirror base provide input of data about flight device travel speed into control-computing unit. This data is taken into consideration when outputting control signals to head mirror actuators. ^ EFFECT: improvement of pointing accuracy. ^ 3 cl, 1 dwg |
| format | Patent |
| fullrecord | <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_RU2335728C1</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>RU2335728C1</sourcerecordid><originalsourceid>FETCH-epo_espacenet_RU2335728C13</originalsourceid><addsrcrecordid>eNrjZND1DwjxdHb00XX1cXUOCfL383RWCHZ1DHL2UHD0c1EICXJ09vb0c1cIjgwOcfXlYWBNS8wpTuWF0twMCm6uIc4euqkF-fGpxQWJyal5qSXxQaFGxsam5kYWzobGRCgBAHzFJUI</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>OPTICAL-ELECTRONIC SEARCH AND TRACKING SYSTEM</title><source>esp@cenet</source><creator>KHISAMOV RAMIS SHARAFOVICH ; BELOZEROV AL'BERT FEDOROVICH ; DOBRYNIN ALEKSANDR ALEKSANDROVICH ; PRIKHOD'KO VIKTOR NIKITOVICH ; IVANOV VLADIMIR PETROVICH ; SUNTSOV VLADIMIR VJACHESLAVOVICH ; BALOEV VILLEN ARNOL'DOVICH ; JATSYK VLADIMIR SAMUILOVICH ; ALEKSEEV JURIJ VITAL'EVICH ; VAKHITOV MURAT AKHMETOVICH ; DOROFEEVA MARGARITA VASIL'EVNA</creator><creatorcontrib>KHISAMOV RAMIS SHARAFOVICH ; BELOZEROV AL'BERT FEDOROVICH ; DOBRYNIN ALEKSANDR ALEKSANDROVICH ; PRIKHOD'KO VIKTOR NIKITOVICH ; IVANOV VLADIMIR PETROVICH ; SUNTSOV VLADIMIR VJACHESLAVOVICH ; BALOEV VILLEN ARNOL'DOVICH ; JATSYK VLADIMIR SAMUILOVICH ; ALEKSEEV JURIJ VITAL'EVICH ; VAKHITOV MURAT AKHMETOVICH ; DOROFEEVA MARGARITA VASIL'EVNA</creatorcontrib><description>FIELD: transportation, physics. ^ SUBSTANCE: invention relates to defence of aircraft planes (AP) for jamming by infrared target-seeking devices of attacking missles (ITSD). System contains head mirror, movable along two mutually perpendicular axes and provided with aspect sensors, infrared (IR) direction-finding channel containing lens and photodetector (FD). Between the head mirror and lens at an angle to optical axis fixed flat mirror with axial hole is installed. The hole is positioned at laser emission path from transmitting laser channel. FD output and outputs of head mirror aspect sensors are connected to control-computing unit, control outputs of which are connected to head mirror actuators and to control input of transmitting laser channel. Lens is made of two components between which, in focal plane of the first on emission path component, aperture is installed which prevents diffused laser emission from getting on FD array. At the same time, IR direction-finding channel is receiving laser channel of the system. Determination of error angle between system optical axis and laser signal reflected by target in IR direction-finding channel provides improvement of accuracy of laser emission pointing at ITSD of attacking missiles. Angular-rate sensors installed on head mirror base provide input of data about flight device travel speed into control-computing unit. This data is taken into consideration when outputting control signals to head mirror actuators. ^ EFFECT: improvement of pointing accuracy. ^ 3 cl, 1 dwg</description><language>eng ; rus</language><subject>AIMING ; BLASTING ; HEATING ; LIGHTING ; MEASURING ; MEASURING ANGLES ; MEASURING AREAS ; MEASURING IRREGULARITIES OF SURFACES OR CONTOURS ; MEASURING LENGTH, THICKNESS OR SIMILAR LINEARDIMENSIONS ; MECHANICAL ENGINEERING ; PHYSICS ; TESTING ; WEAPON SIGHTS ; WEAPONS</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=20081010&DB=EPODOC&CC=RU&NR=2335728C1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25543,76293</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20081010&DB=EPODOC&CC=RU&NR=2335728C1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>KHISAMOV RAMIS SHARAFOVICH</creatorcontrib><creatorcontrib>BELOZEROV AL'BERT FEDOROVICH</creatorcontrib><creatorcontrib>DOBRYNIN ALEKSANDR ALEKSANDROVICH</creatorcontrib><creatorcontrib>PRIKHOD'KO VIKTOR NIKITOVICH</creatorcontrib><creatorcontrib>IVANOV VLADIMIR PETROVICH</creatorcontrib><creatorcontrib>SUNTSOV VLADIMIR VJACHESLAVOVICH</creatorcontrib><creatorcontrib>BALOEV VILLEN ARNOL'DOVICH</creatorcontrib><creatorcontrib>JATSYK VLADIMIR SAMUILOVICH</creatorcontrib><creatorcontrib>ALEKSEEV JURIJ VITAL'EVICH</creatorcontrib><creatorcontrib>VAKHITOV MURAT AKHMETOVICH</creatorcontrib><creatorcontrib>DOROFEEVA MARGARITA VASIL'EVNA</creatorcontrib><title>OPTICAL-ELECTRONIC SEARCH AND TRACKING SYSTEM</title><description>FIELD: transportation, physics. ^ SUBSTANCE: invention relates to defence of aircraft planes (AP) for jamming by infrared target-seeking devices of attacking missles (ITSD). System contains head mirror, movable along two mutually perpendicular axes and provided with aspect sensors, infrared (IR) direction-finding channel containing lens and photodetector (FD). Between the head mirror and lens at an angle to optical axis fixed flat mirror with axial hole is installed. The hole is positioned at laser emission path from transmitting laser channel. FD output and outputs of head mirror aspect sensors are connected to control-computing unit, control outputs of which are connected to head mirror actuators and to control input of transmitting laser channel. Lens is made of two components between which, in focal plane of the first on emission path component, aperture is installed which prevents diffused laser emission from getting on FD array. At the same time, IR direction-finding channel is receiving laser channel of the system. Determination of error angle between system optical axis and laser signal reflected by target in IR direction-finding channel provides improvement of accuracy of laser emission pointing at ITSD of attacking missiles. Angular-rate sensors installed on head mirror base provide input of data about flight device travel speed into control-computing unit. This data is taken into consideration when outputting control signals to head mirror actuators. ^ EFFECT: improvement of pointing accuracy. ^ 3 cl, 1 dwg</description><subject>AIMING</subject><subject>BLASTING</subject><subject>HEATING</subject><subject>LIGHTING</subject><subject>MEASURING</subject><subject>MEASURING ANGLES</subject><subject>MEASURING AREAS</subject><subject>MEASURING IRREGULARITIES OF SURFACES OR CONTOURS</subject><subject>MEASURING LENGTH, THICKNESS OR SIMILAR LINEARDIMENSIONS</subject><subject>MECHANICAL ENGINEERING</subject><subject>PHYSICS</subject><subject>TESTING</subject><subject>WEAPON SIGHTS</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2008</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZND1DwjxdHb00XX1cXUOCfL383RWCHZ1DHL2UHD0c1EICXJ09vb0c1cIjgwOcfXlYWBNS8wpTuWF0twMCm6uIc4euqkF-fGpxQWJyal5qSXxQaFGxsam5kYWzobGRCgBAHzFJUI</recordid><startdate>20081010</startdate><enddate>20081010</enddate><creator>KHISAMOV RAMIS SHARAFOVICH</creator><creator>BELOZEROV AL'BERT FEDOROVICH</creator><creator>DOBRYNIN ALEKSANDR ALEKSANDROVICH</creator><creator>PRIKHOD'KO VIKTOR NIKITOVICH</creator><creator>IVANOV VLADIMIR PETROVICH</creator><creator>SUNTSOV VLADIMIR VJACHESLAVOVICH</creator><creator>BALOEV VILLEN ARNOL'DOVICH</creator><creator>JATSYK VLADIMIR SAMUILOVICH</creator><creator>ALEKSEEV JURIJ VITAL'EVICH</creator><creator>VAKHITOV MURAT AKHMETOVICH</creator><creator>DOROFEEVA MARGARITA VASIL'EVNA</creator><scope>EVB</scope></search><sort><creationdate>20081010</creationdate><title>OPTICAL-ELECTRONIC SEARCH AND TRACKING SYSTEM</title><author>KHISAMOV RAMIS SHARAFOVICH ; BELOZEROV AL'BERT FEDOROVICH ; DOBRYNIN ALEKSANDR ALEKSANDROVICH ; PRIKHOD'KO VIKTOR NIKITOVICH ; IVANOV VLADIMIR PETROVICH ; SUNTSOV VLADIMIR VJACHESLAVOVICH ; BALOEV VILLEN ARNOL'DOVICH ; JATSYK VLADIMIR SAMUILOVICH ; ALEKSEEV JURIJ VITAL'EVICH ; VAKHITOV MURAT AKHMETOVICH ; DOROFEEVA MARGARITA VASIL'EVNA</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_RU2335728C13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; rus</language><creationdate>2008</creationdate><topic>AIMING</topic><topic>BLASTING</topic><topic>HEATING</topic><topic>LIGHTING</topic><topic>MEASURING</topic><topic>MEASURING ANGLES</topic><topic>MEASURING AREAS</topic><topic>MEASURING IRREGULARITIES OF SURFACES OR CONTOURS</topic><topic>MEASURING LENGTH, THICKNESS OR SIMILAR LINEARDIMENSIONS</topic><topic>MECHANICAL ENGINEERING</topic><topic>PHYSICS</topic><topic>TESTING</topic><topic>WEAPON SIGHTS</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>KHISAMOV RAMIS SHARAFOVICH</creatorcontrib><creatorcontrib>BELOZEROV AL'BERT FEDOROVICH</creatorcontrib><creatorcontrib>DOBRYNIN ALEKSANDR ALEKSANDROVICH</creatorcontrib><creatorcontrib>PRIKHOD'KO VIKTOR NIKITOVICH</creatorcontrib><creatorcontrib>IVANOV VLADIMIR PETROVICH</creatorcontrib><creatorcontrib>SUNTSOV VLADIMIR VJACHESLAVOVICH</creatorcontrib><creatorcontrib>BALOEV VILLEN ARNOL'DOVICH</creatorcontrib><creatorcontrib>JATSYK VLADIMIR SAMUILOVICH</creatorcontrib><creatorcontrib>ALEKSEEV JURIJ VITAL'EVICH</creatorcontrib><creatorcontrib>VAKHITOV MURAT AKHMETOVICH</creatorcontrib><creatorcontrib>DOROFEEVA MARGARITA VASIL'EVNA</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>KHISAMOV RAMIS SHARAFOVICH</au><au>BELOZEROV AL'BERT FEDOROVICH</au><au>DOBRYNIN ALEKSANDR ALEKSANDROVICH</au><au>PRIKHOD'KO VIKTOR NIKITOVICH</au><au>IVANOV VLADIMIR PETROVICH</au><au>SUNTSOV VLADIMIR VJACHESLAVOVICH</au><au>BALOEV VILLEN ARNOL'DOVICH</au><au>JATSYK VLADIMIR SAMUILOVICH</au><au>ALEKSEEV JURIJ VITAL'EVICH</au><au>VAKHITOV MURAT AKHMETOVICH</au><au>DOROFEEVA MARGARITA VASIL'EVNA</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>OPTICAL-ELECTRONIC SEARCH AND TRACKING SYSTEM</title><date>2008-10-10</date><risdate>2008</risdate><abstract>FIELD: transportation, physics. ^ SUBSTANCE: invention relates to defence of aircraft planes (AP) for jamming by infrared target-seeking devices of attacking missles (ITSD). System contains head mirror, movable along two mutually perpendicular axes and provided with aspect sensors, infrared (IR) direction-finding channel containing lens and photodetector (FD). Between the head mirror and lens at an angle to optical axis fixed flat mirror with axial hole is installed. The hole is positioned at laser emission path from transmitting laser channel. FD output and outputs of head mirror aspect sensors are connected to control-computing unit, control outputs of which are connected to head mirror actuators and to control input of transmitting laser channel. Lens is made of two components between which, in focal plane of the first on emission path component, aperture is installed which prevents diffused laser emission from getting on FD array. At the same time, IR direction-finding channel is receiving laser channel of the system. Determination of error angle between system optical axis and laser signal reflected by target in IR direction-finding channel provides improvement of accuracy of laser emission pointing at ITSD of attacking missiles. Angular-rate sensors installed on head mirror base provide input of data about flight device travel speed into control-computing unit. This data is taken into consideration when outputting control signals to head mirror actuators. ^ EFFECT: improvement of pointing accuracy. ^ 3 cl, 1 dwg</abstract><oa>free_for_read</oa></addata></record> |
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| subjects | AIMING BLASTING HEATING LIGHTING MEASURING MEASURING ANGLES MEASURING AREAS MEASURING IRREGULARITIES OF SURFACES OR CONTOURS MEASURING LENGTH, THICKNESS OR SIMILAR LINEARDIMENSIONS MECHANICAL ENGINEERING PHYSICS TESTING WEAPON SIGHTS WEAPONS |
| title | OPTICAL-ELECTRONIC SEARCH AND TRACKING SYSTEM |
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