Unmanned aerial vehicle-mounted warplane radar target drone

Unmanned aerial vehicle-mounted warplane radar target drone

The invention discloses an unmanned aerial vehicle-mounted warplane radar target drone, which comprises a nose direction typical characteristic simulation assembly, a wing direction typical characteristic simulation assembly and a tail direction typical characteristic simulation assembly, and relate...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Hauptverfasser: WANG YIFENG, WANG XUETIAN, HAO JIAXING
Format: Patent
Sprache:chi ; eng
Schlagworte:
BLASTING
BULLET CATCHERS
HEATING
LIGHTING
MECHANICAL ENGINEERING
TARGET RANGES
TARGETS
WEAPONS
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 WANG YIFENG
WANG XUETIAN
HAO JIAXING
description The invention discloses an unmanned aerial vehicle-mounted warplane radar target drone, which comprises a nose direction typical characteristic simulation assembly, a wing direction typical characteristic simulation assembly and a tail direction typical characteristic simulation assembly, and relates to the technical field of radar target drones. According to the simulation assembly for the typical characteristics of the directions of the nose, the wings and the tail of the unmanned aerial vehicle-mounted fighter radar target drone, simulation of narrow airspace peak characteristics in fighter airspace RCS distribution characteristics can be realized through the 60-degree variable angle reflector, and simulation of stable spatial distribution characteristics in the fighter airspace RCS distribution characteristics can be realized through the Luneberg ball; and by combining with the 60-degree variable-angle reflector, the simulation of fluctuation characteristics among multiple scatterers and multiple reflecto
format Patent
fullrecord <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_CN117824435A</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>CN117824435A</sourcerecordid><originalsourceid>FETCH-epo_espacenet_CN117824435A3</originalsourceid><addsrcrecordid>eNrjZLAOzctNzMtLTVFITC3KTMxRKEvNyEzOSdXNzS_NKwEKlycWFeQk5qUqFCWmJBYplCQWpaeWKKQU5eel8jCwpiXmFKfyQmluBkU31xBnD93Ugvz41OKCxOTUvNSSeGc_Q0NzCyMTE2NTR2Ni1AAAw1wvmA</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>Unmanned aerial vehicle-mounted warplane radar target drone</title><source>esp@cenet</source><creator>WANG YIFENG ; WANG XUETIAN ; HAO JIAXING</creator><creatorcontrib>WANG YIFENG ; WANG XUETIAN ; HAO JIAXING</creatorcontrib><description>The invention discloses an unmanned aerial vehicle-mounted warplane radar target drone, which comprises a nose direction typical characteristic simulation assembly, a wing direction typical characteristic simulation assembly and a tail direction typical characteristic simulation assembly, and relates to the technical field of radar target drones. According to the simulation assembly for the typical characteristics of the directions of the nose, the wings and the tail of the unmanned aerial vehicle-mounted fighter radar target drone, simulation of narrow airspace peak characteristics in fighter airspace RCS distribution characteristics can be realized through the 60-degree variable angle reflector, and simulation of stable spatial distribution characteristics in the fighter airspace RCS distribution characteristics can be realized through the Luneberg ball; and by combining with the 60-degree variable-angle reflector, the simulation of fluctuation characteristics among multiple scatterers and multiple reflecto</description><language>chi ; eng</language><subject>BLASTING ; BULLET CATCHERS ; HEATING ; LIGHTING ; MECHANICAL ENGINEERING ; TARGET RANGES ; TARGETS ; WEAPONS</subject><creationdate>2024</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=20240405&amp;DB=EPODOC&amp;CC=CN&amp;NR=117824435A$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76419</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&amp;date=20240405&amp;DB=EPODOC&amp;CC=CN&amp;NR=117824435A$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>WANG YIFENG</creatorcontrib><creatorcontrib>WANG XUETIAN</creatorcontrib><creatorcontrib>HAO JIAXING</creatorcontrib><title>Unmanned aerial vehicle-mounted warplane radar target drone</title><description>The invention discloses an unmanned aerial vehicle-mounted warplane radar target drone, which comprises a nose direction typical characteristic simulation assembly, a wing direction typical characteristic simulation assembly and a tail direction typical characteristic simulation assembly, and relates to the technical field of radar target drones. According to the simulation assembly for the typical characteristics of the directions of the nose, the wings and the tail of the unmanned aerial vehicle-mounted fighter radar target drone, simulation of narrow airspace peak characteristics in fighter airspace RCS distribution characteristics can be realized through the 60-degree variable angle reflector, and simulation of stable spatial distribution characteristics in the fighter airspace RCS distribution characteristics can be realized through the Luneberg ball; and by combining with the 60-degree variable-angle reflector, the simulation of fluctuation characteristics among multiple scatterers and multiple reflecto</description><subject>BLASTING</subject><subject>BULLET CATCHERS</subject><subject>HEATING</subject><subject>LIGHTING</subject><subject>MECHANICAL ENGINEERING</subject><subject>TARGET RANGES</subject><subject>TARGETS</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2024</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZLAOzctNzMtLTVFITC3KTMxRKEvNyEzOSdXNzS_NKwEKlycWFeQk5qUqFCWmJBYplCQWpaeWKKQU5eel8jCwpiXmFKfyQmluBkU31xBnD93Ugvz41OKCxOTUvNSSeGc_Q0NzCyMTE2NTR2Ni1AAAw1wvmA</recordid><startdate>20240405</startdate><enddate>20240405</enddate><creator>WANG YIFENG</creator><creator>WANG XUETIAN</creator><creator>HAO JIAXING</creator><scope>EVB</scope></search><sort><creationdate>20240405</creationdate><title>Unmanned aerial vehicle-mounted warplane radar target drone</title><author>WANG YIFENG ; WANG XUETIAN ; HAO JIAXING</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_CN117824435A3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>chi ; eng</language><creationdate>2024</creationdate><topic>BLASTING</topic><topic>BULLET CATCHERS</topic><topic>HEATING</topic><topic>LIGHTING</topic><topic>MECHANICAL ENGINEERING</topic><topic>TARGET RANGES</topic><topic>TARGETS</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>WANG YIFENG</creatorcontrib><creatorcontrib>WANG XUETIAN</creatorcontrib><creatorcontrib>HAO JIAXING</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>WANG YIFENG</au><au>WANG XUETIAN</au><au>HAO JIAXING</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Unmanned aerial vehicle-mounted warplane radar target drone</title><date>2024-04-05</date><risdate>2024</risdate><abstract>The invention discloses an unmanned aerial vehicle-mounted warplane radar target drone, which comprises a nose direction typical characteristic simulation assembly, a wing direction typical characteristic simulation assembly and a tail direction typical characteristic simulation assembly, and relates to the technical field of radar target drones. According to the simulation assembly for the typical characteristics of the directions of the nose, the wings and the tail of the unmanned aerial vehicle-mounted fighter radar target drone, simulation of narrow airspace peak characteristics in fighter airspace RCS distribution characteristics can be realized through the 60-degree variable angle reflector, and simulation of stable spatial distribution characteristics in the fighter airspace RCS distribution characteristics can be realized through the Luneberg ball; and by combining with the 60-degree variable-angle reflector, the simulation of fluctuation characteristics among multiple scatterers and multiple reflecto</abstract><oa>free_for_read</oa></addata></record>
fulltext fulltext_linktorsrc
identifier
ispartof
issn
language chi ; eng
recordid cdi_epo_espacenet_CN117824435A
source esp@cenet
subjects BLASTING
BULLET CATCHERS
HEATING
LIGHTING
MECHANICAL ENGINEERING
TARGET RANGES
TARGETS
WEAPONS
title Unmanned aerial vehicle-mounted warplane radar target drone
url https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-07T15%3A59%3A34IST&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=WANG%20YIFENG&rft.date=2024-04-05&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3ECN117824435A%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