MONOPULSE TRACKING METHOD AND SYSTEM BASED ON MULTI STATE MODE
According to an embodiment of the present invention, provided is a monopulse satellite tracking method based on a multi-state mode, which includes the steps of: receiving satellite signals from a satellite and multi-channel signals from an antenna by an antenna control panel; outputting an error ang...
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| creator | LEE DONG HYEOK KIM JAE SIN NOH SUNG MIN |
| description | According to an embodiment of the present invention, provided is a monopulse satellite tracking method based on a multi-state mode, which includes the steps of: receiving satellite signals from a satellite and multi-channel signals from an antenna by an antenna control panel; outputting an error angle based on the multi-channel signal by the antenna control panel; outputting a beam angle of the antenna by performing a transition algorithm for switching between a plurality of individual modes based on the satellite signal and the multi-channel signal by the antenna control panel; and controlling the driving of the antenna based on the beam angle by an antenna driving panel. Therefore, the continuity and stability of satellite tracking can be secured.
본 발명의 일 실시예에 따른 다중 상태 모드 기반의 모노펄스 위성 추적 방법은 안테나 제어반에 의해 위성으로부터 위성신호 및 안테나로부터 다채널 신호를 수신하는 단계; 상기 안테나 제어반에 의해 상기 다채널 신호를 기초로 오차각을 출력하는 단계; 상기 안테나 제어반에 의해 상기 위성신호 및 상기 다채널 신호를 기초로 복수의 개별 모드들 간의 전환을 수행하는 천이 알고리즘을 수행하여 안테나의 지향각을 출력하는 단계; 및 안테나 구동반에 의해 상기 지향각을 기초로 안테나의 구동을 제어하는 단계;를 포함한다. |
| format | Patent |
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본 발명의 일 실시예에 따른 다중 상태 모드 기반의 모노펄스 위성 추적 방법은 안테나 제어반에 의해 위성으로부터 위성신호 및 안테나로부터 다채널 신호를 수신하는 단계; 상기 안테나 제어반에 의해 상기 다채널 신호를 기초로 오차각을 출력하는 단계; 상기 안테나 제어반에 의해 상기 위성신호 및 상기 다채널 신호를 기초로 복수의 개별 모드들 간의 전환을 수행하는 천이 알고리즘을 수행하여 안테나의 지향각을 출력하는 단계; 및 안테나 구동반에 의해 상기 지향각을 기초로 안테나의 구동을 제어하는 단계;를 포함한다.</description><language>eng ; kor</language><subject>ANALOGOUS ARRANGEMENTS USING OTHER WAVES ; ANTENNAS, i.e. RADIO AERIALS ; BASIC ELECTRIC ELEMENTS ; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES ; ELECTRICITY ; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION ORRERADIATION OF RADIO WAVES ; MEASURING ; PHYSICS ; RADIO DIRECTION-FINDING ; RADIO NAVIGATION ; TESTING</subject><creationdate>2023</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=20230801&DB=EPODOC&CC=KR&NR=20230114622A$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25563,76418</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20230801&DB=EPODOC&CC=KR&NR=20230114622A$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>LEE DONG HYEOK</creatorcontrib><creatorcontrib>KIM JAE SIN</creatorcontrib><creatorcontrib>NOH SUNG MIN</creatorcontrib><title>MONOPULSE TRACKING METHOD AND SYSTEM BASED ON MULTI STATE MODE</title><description>According to an embodiment of the present invention, provided is a monopulse satellite tracking method based on a multi-state mode, which includes the steps of: receiving satellite signals from a satellite and multi-channel signals from an antenna by an antenna control panel; outputting an error angle based on the multi-channel signal by the antenna control panel; outputting a beam angle of the antenna by performing a transition algorithm for switching between a plurality of individual modes based on the satellite signal and the multi-channel signal by the antenna control panel; and controlling the driving of the antenna based on the beam angle by an antenna driving panel. Therefore, the continuity and stability of satellite tracking can be secured.
본 발명의 일 실시예에 따른 다중 상태 모드 기반의 모노펄스 위성 추적 방법은 안테나 제어반에 의해 위성으로부터 위성신호 및 안테나로부터 다채널 신호를 수신하는 단계; 상기 안테나 제어반에 의해 상기 다채널 신호를 기초로 오차각을 출력하는 단계; 상기 안테나 제어반에 의해 상기 위성신호 및 상기 다채널 신호를 기초로 복수의 개별 모드들 간의 전환을 수행하는 천이 알고리즘을 수행하여 안테나의 지향각을 출력하는 단계; 및 안테나 구동반에 의해 상기 지향각을 기초로 안테나의 구동을 제어하는 단계;를 포함한다.</description><subject>ANALOGOUS ARRANGEMENTS USING OTHER WAVES</subject><subject>ANTENNAS, i.e. RADIO AERIALS</subject><subject>BASIC ELECTRIC ELEMENTS</subject><subject>DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES</subject><subject>ELECTRICITY</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>2023</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZLDz9ffzDwj1CXZVCAlydPb29HNX8HUN8fB3UXD0c1EIjgwOcfVVcHIMdnVR8PdT8A31CfFUCA5xDHFV8PV3ceVhYE1LzClO5YXS3AzKbq4hzh66qQX58anFBYnJqXmpJfHeQUYGRsYGhoYmZkZGjsbEqQIA-Mwqyg</recordid><startdate>20230801</startdate><enddate>20230801</enddate><creator>LEE DONG HYEOK</creator><creator>KIM JAE SIN</creator><creator>NOH SUNG MIN</creator><scope>EVB</scope></search><sort><creationdate>20230801</creationdate><title>MONOPULSE TRACKING METHOD AND SYSTEM BASED ON MULTI STATE MODE</title><author>LEE DONG HYEOK ; KIM JAE SIN ; NOH SUNG MIN</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_KR20230114622A3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; kor</language><creationdate>2023</creationdate><topic>ANALOGOUS ARRANGEMENTS USING OTHER WAVES</topic><topic>ANTENNAS, i.e. RADIO AERIALS</topic><topic>BASIC ELECTRIC ELEMENTS</topic><topic>DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES</topic><topic>ELECTRICITY</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>LEE DONG HYEOK</creatorcontrib><creatorcontrib>KIM JAE SIN</creatorcontrib><creatorcontrib>NOH SUNG MIN</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>LEE DONG HYEOK</au><au>KIM JAE SIN</au><au>NOH SUNG MIN</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>MONOPULSE TRACKING METHOD AND SYSTEM BASED ON MULTI STATE MODE</title><date>2023-08-01</date><risdate>2023</risdate><abstract>According to an embodiment of the present invention, provided is a monopulse satellite tracking method based on a multi-state mode, which includes the steps of: receiving satellite signals from a satellite and multi-channel signals from an antenna by an antenna control panel; outputting an error angle based on the multi-channel signal by the antenna control panel; outputting a beam angle of the antenna by performing a transition algorithm for switching between a plurality of individual modes based on the satellite signal and the multi-channel signal by the antenna control panel; and controlling the driving of the antenna based on the beam angle by an antenna driving panel. Therefore, the continuity and stability of satellite tracking can be secured.
본 발명의 일 실시예에 따른 다중 상태 모드 기반의 모노펄스 위성 추적 방법은 안테나 제어반에 의해 위성으로부터 위성신호 및 안테나로부터 다채널 신호를 수신하는 단계; 상기 안테나 제어반에 의해 상기 다채널 신호를 기초로 오차각을 출력하는 단계; 상기 안테나 제어반에 의해 상기 위성신호 및 상기 다채널 신호를 기초로 복수의 개별 모드들 간의 전환을 수행하는 천이 알고리즘을 수행하여 안테나의 지향각을 출력하는 단계; 및 안테나 구동반에 의해 상기 지향각을 기초로 안테나의 구동을 제어하는 단계;를 포함한다.</abstract><oa>free_for_read</oa></addata></record> |
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| subjects | ANALOGOUS ARRANGEMENTS USING OTHER WAVES ANTENNAS, i.e. RADIO AERIALS BASIC ELECTRIC ELEMENTS DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES ELECTRICITY LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION ORRERADIATION OF RADIO WAVES MEASURING PHYSICS RADIO DIRECTION-FINDING RADIO NAVIGATION TESTING |
| title | MONOPULSE TRACKING METHOD AND SYSTEM BASED ON MULTI STATE MODE |
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