Unmanned aerial vehicle accurate bomb throwing method

The invention aims at providing a method for analyzing the motion path of a bomb thrown by an unmanned aerial vehicle, the actual motion path of the bomb body can be analyzed by utilizing the actually measured data such as the wind speed, the flight speed of the unmanned aerial vehicle and the heigh...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Hauptverfasser: QUAN MING, CHEN WEIHUA, GUO HANGSHEN, LUO NAIXIN, LI XIA
Format: Patent
Sprache:chi ; 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 QUAN MING
CHEN WEIHUA
GUO HANGSHEN
LUO NAIXIN
LI XIA
description The invention aims at providing a method for analyzing the motion path of a bomb thrown by an unmanned aerial vehicle, the actual motion path of the bomb body can be analyzed by utilizing the actually measured data such as the wind speed, the flight speed of the unmanned aerial vehicle and the height of the bomb throwing point, and the bomb throwing angle of the unmanned aerial vehicle can be adjusted in real time. According to the method, the motion path of the bomb thrown by the unmanned aerial vehicle can be rapidly predicted according to the measured real-time wind speed, the bomb throwing angle of the unmanned aerial vehicle is adjusted through information interaction between unmanned aerial vehicle groups, and the bomb throwing accuracy is improved. Compared with the prior art, the method has the advantages that the bomb throwing angle can be set according to the actually measured wind speed and the flight speed of the unmanned aerial vehicle, and the motion path of bomb throwing is analyzed; and by uti
format Patent
fullrecord <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_CN112706925A</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>CN112706925A</sourcerecordid><originalsourceid>FETCH-epo_espacenet_CN112706925A3</originalsourceid><addsrcrecordid>eNrjZDANzctNzMtLTVFITC3KTMxRKEvNyEzOSVVITE4uLUosSVVIys9NUijJKMovz8xLV8hNLcnIT-FhYE1LzClO5YXS3AyKbq4hzh66qQX58anFBYnJqXmpJfHOfoaGRuYGZpZGpo7GxKgBAGyTLT0</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>Unmanned aerial vehicle accurate bomb throwing method</title><source>esp@cenet</source><creator>QUAN MING ; CHEN WEIHUA ; GUO HANGSHEN ; LUO NAIXIN ; LI XIA</creator><creatorcontrib>QUAN MING ; CHEN WEIHUA ; GUO HANGSHEN ; LUO NAIXIN ; LI XIA</creatorcontrib><description>The invention aims at providing a method for analyzing the motion path of a bomb thrown by an unmanned aerial vehicle, the actual motion path of the bomb body can be analyzed by utilizing the actually measured data such as the wind speed, the flight speed of the unmanned aerial vehicle and the height of the bomb throwing point, and the bomb throwing angle of the unmanned aerial vehicle can be adjusted in real time. According to the method, the motion path of the bomb thrown by the unmanned aerial vehicle can be rapidly predicted according to the measured real-time wind speed, the bomb throwing angle of the unmanned aerial vehicle is adjusted through information interaction between unmanned aerial vehicle groups, and the bomb throwing accuracy is improved. Compared with the prior art, the method has the advantages that the bomb throwing angle can be set according to the actually measured wind speed and the flight speed of the unmanned aerial vehicle, and the motion path of bomb throwing is analyzed; and by uti</description><language>chi ; eng</language><subject>AIRCRAFT ; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT ; AVIATION ; COSMONAUTICS ; EQUIPMENT FOR FITTING IN OR TO AIRCRAFT ; FLYING SUITS ; PARACHUTES ; PERFORMING OPERATIONS ; TRANSPORTING</subject><creationdate>2021</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=20210427&amp;DB=EPODOC&amp;CC=CN&amp;NR=112706925A$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,777,882,25545,76296</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&amp;date=20210427&amp;DB=EPODOC&amp;CC=CN&amp;NR=112706925A$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>QUAN MING</creatorcontrib><creatorcontrib>CHEN WEIHUA</creatorcontrib><creatorcontrib>GUO HANGSHEN</creatorcontrib><creatorcontrib>LUO NAIXIN</creatorcontrib><creatorcontrib>LI XIA</creatorcontrib><title>Unmanned aerial vehicle accurate bomb throwing method</title><description>The invention aims at providing a method for analyzing the motion path of a bomb thrown by an unmanned aerial vehicle, the actual motion path of the bomb body can be analyzed by utilizing the actually measured data such as the wind speed, the flight speed of the unmanned aerial vehicle and the height of the bomb throwing point, and the bomb throwing angle of the unmanned aerial vehicle can be adjusted in real time. According to the method, the motion path of the bomb thrown by the unmanned aerial vehicle can be rapidly predicted according to the measured real-time wind speed, the bomb throwing angle of the unmanned aerial vehicle is adjusted through information interaction between unmanned aerial vehicle groups, and the bomb throwing accuracy is improved. Compared with the prior art, the method has the advantages that the bomb throwing angle can be set according to the actually measured wind speed and the flight speed of the unmanned aerial vehicle, and the motion path of bomb throwing is analyzed; and by uti</description><subject>AIRCRAFT</subject><subject>ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT</subject><subject>AVIATION</subject><subject>COSMONAUTICS</subject><subject>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</subject><subject>FLYING SUITS</subject><subject>PARACHUTES</subject><subject>PERFORMING OPERATIONS</subject><subject>TRANSPORTING</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2021</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZDANzctNzMtLTVFITC3KTMxRKEvNyEzOSVVITE4uLUosSVVIys9NUijJKMovz8xLV8hNLcnIT-FhYE1LzClO5YXS3AyKbq4hzh66qQX58anFBYnJqXmpJfHOfoaGRuYGZpZGpo7GxKgBAGyTLT0</recordid><startdate>20210427</startdate><enddate>20210427</enddate><creator>QUAN MING</creator><creator>CHEN WEIHUA</creator><creator>GUO HANGSHEN</creator><creator>LUO NAIXIN</creator><creator>LI XIA</creator><scope>EVB</scope></search><sort><creationdate>20210427</creationdate><title>Unmanned aerial vehicle accurate bomb throwing method</title><author>QUAN MING ; CHEN WEIHUA ; GUO HANGSHEN ; LUO NAIXIN ; LI XIA</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_CN112706925A3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>chi ; eng</language><creationdate>2021</creationdate><topic>AIRCRAFT</topic><topic>ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT</topic><topic>AVIATION</topic><topic>COSMONAUTICS</topic><topic>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</topic><topic>FLYING SUITS</topic><topic>PARACHUTES</topic><topic>PERFORMING OPERATIONS</topic><topic>TRANSPORTING</topic><toplevel>online_resources</toplevel><creatorcontrib>QUAN MING</creatorcontrib><creatorcontrib>CHEN WEIHUA</creatorcontrib><creatorcontrib>GUO HANGSHEN</creatorcontrib><creatorcontrib>LUO NAIXIN</creatorcontrib><creatorcontrib>LI XIA</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>QUAN MING</au><au>CHEN WEIHUA</au><au>GUO HANGSHEN</au><au>LUO NAIXIN</au><au>LI XIA</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Unmanned aerial vehicle accurate bomb throwing method</title><date>2021-04-27</date><risdate>2021</risdate><abstract>The invention aims at providing a method for analyzing the motion path of a bomb thrown by an unmanned aerial vehicle, the actual motion path of the bomb body can be analyzed by utilizing the actually measured data such as the wind speed, the flight speed of the unmanned aerial vehicle and the height of the bomb throwing point, and the bomb throwing angle of the unmanned aerial vehicle can be adjusted in real time. According to the method, the motion path of the bomb thrown by the unmanned aerial vehicle can be rapidly predicted according to the measured real-time wind speed, the bomb throwing angle of the unmanned aerial vehicle is adjusted through information interaction between unmanned aerial vehicle groups, and the bomb throwing accuracy is improved. Compared with the prior art, the method has the advantages that the bomb throwing angle can be set according to the actually measured wind speed and the flight speed of the unmanned aerial vehicle, and the motion path of bomb throwing is analyzed; and by uti</abstract><oa>free_for_read</oa></addata></record>
fulltext fulltext_linktorsrc
identifier
ispartof
issn
language chi ; eng
recordid cdi_epo_espacenet_CN112706925A
source esp@cenet
subjects AIRCRAFT
ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT
AVIATION
COSMONAUTICS
EQUIPMENT FOR FITTING IN OR TO AIRCRAFT
FLYING SUITS
PARACHUTES
PERFORMING OPERATIONS
TRANSPORTING
title Unmanned aerial vehicle accurate bomb throwing method
url https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-18T19%3A35%3A42IST&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=QUAN%20MING&rft.date=2021-04-27&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3ECN112706925A%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