Rocket launching control system
The invention discloses a rocket launching control system. Specifically, a boosting power supply is connected to one end of a boosting capacitor, the other end of the boosting capacitor is grounded, and a first current limiting resistor is connected with the boosting capacitor in parallel; the boost...
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| creator | ZHENG BOHUA SUN YONGTAO JIN LYUSHENG QIAO HONGXIA CHENG TAO LI HUIFANG ZHANG XIAOHANG LI JIAN WEI XUHUI ZHANG BAOCHUN WANG XIAOXIA GAN LU LI LING ZHU SIHUA FAN YANPING LIU XIAO JIA XIADONG GUO HUA GU KANGLE HANG JIA |
| description | The invention discloses a rocket launching control system. Specifically, a boosting power supply is connected to one end of a boosting capacitor, the other end of the boosting capacitor is grounded, and a first current limiting resistor is connected with the boosting capacitor in parallel; the boosting power supply is accessed to a CPU (Central Processing Unit) through a first analog input interface; a launching control power supply is connected to the boosting power supply through a second current limiting resistor and a double-pole and double-throw relay which is connected with a resistance measuring pathway, and a switch of the relay is connected with a firing circuit of a controlled rocket; the resistance measuring pathway is accessed to the CPU through a second analog input interface; the control end of the relay is accessed to the CPU through a DI/DO (Digital Input/Digital Output) interface; a control instruction output from outside is received by the CPU and is transmitted to the control end of a launc |
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| fullrecord | <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_CN105444618A</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>CN105444618A</sourcerecordid><originalsourceid>FETCH-epo_espacenet_CN105444618A3</originalsourceid><addsrcrecordid>eNrjZJAPyk_OTi1RyEkszUvOyMxLV0jOzyspys9RKK4sLknN5WFgTUvMKU7lhdLcDIpuriHOHrqpBfnxqcUFicmpeakl8c5-hgamJiYmZoYWjsbEqAEAQyQlLw</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>Rocket launching control system</title><source>esp@cenet</source><creator>ZHENG BOHUA ; SUN YONGTAO ; JIN LYUSHENG ; QIAO HONGXIA ; CHENG TAO ; LI HUIFANG ; ZHANG XIAOHANG ; LI JIAN ; WEI XUHUI ; ZHANG BAOCHUN ; WANG XIAOXIA ; GAN LU ; LI LING ; ZHU SIHUA ; FAN YANPING ; LIU XIAO ; JIA XIADONG ; GUO HUA ; GU KANGLE ; HANG JIA</creator><creatorcontrib>ZHENG BOHUA ; SUN YONGTAO ; JIN LYUSHENG ; QIAO HONGXIA ; CHENG TAO ; LI HUIFANG ; ZHANG XIAOHANG ; LI JIAN ; WEI XUHUI ; ZHANG BAOCHUN ; WANG XIAOXIA ; GAN LU ; LI LING ; ZHU SIHUA ; FAN YANPING ; LIU XIAO ; JIA XIADONG ; GUO HUA ; GU KANGLE ; HANG JIA</creatorcontrib><description>The invention discloses a rocket launching control system. Specifically, a boosting power supply is connected to one end of a boosting capacitor, the other end of the boosting capacitor is grounded, and a first current limiting resistor is connected with the boosting capacitor in parallel; the boosting power supply is accessed to a CPU (Central Processing Unit) through a first analog input interface; a launching control power supply is connected to the boosting power supply through a second current limiting resistor and a double-pole and double-throw relay which is connected with a resistance measuring pathway, and a switch of the relay is connected with a firing circuit of a controlled rocket; the resistance measuring pathway is accessed to the CPU through a second analog input interface; the control end of the relay is accessed to the CPU through a DI/DO (Digital Input/Digital Output) interface; a control instruction output from outside is received by the CPU and is transmitted to the control end of a launc</description><language>chi ; eng</language><subject>APPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS,e.g. CANNONS ; BLASTING ; HARPOON GUNS ; HEATING ; LAUNCHERS FOR ROCKETS OR TORPEDOES ; LIGHTING ; MECHANICAL ENGINEERING ; WEAPONS</subject><creationdate>2016</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=20160330&DB=EPODOC&CC=CN&NR=105444618A$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25563,76418</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20160330&DB=EPODOC&CC=CN&NR=105444618A$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>ZHENG BOHUA</creatorcontrib><creatorcontrib>SUN YONGTAO</creatorcontrib><creatorcontrib>JIN LYUSHENG</creatorcontrib><creatorcontrib>QIAO HONGXIA</creatorcontrib><creatorcontrib>CHENG TAO</creatorcontrib><creatorcontrib>LI HUIFANG</creatorcontrib><creatorcontrib>ZHANG XIAOHANG</creatorcontrib><creatorcontrib>LI JIAN</creatorcontrib><creatorcontrib>WEI XUHUI</creatorcontrib><creatorcontrib>ZHANG BAOCHUN</creatorcontrib><creatorcontrib>WANG XIAOXIA</creatorcontrib><creatorcontrib>GAN LU</creatorcontrib><creatorcontrib>LI LING</creatorcontrib><creatorcontrib>ZHU SIHUA</creatorcontrib><creatorcontrib>FAN YANPING</creatorcontrib><creatorcontrib>LIU XIAO</creatorcontrib><creatorcontrib>JIA XIADONG</creatorcontrib><creatorcontrib>GUO HUA</creatorcontrib><creatorcontrib>GU KANGLE</creatorcontrib><creatorcontrib>HANG JIA</creatorcontrib><title>Rocket launching control system</title><description>The invention discloses a rocket launching control system. Specifically, a boosting power supply is connected to one end of a boosting capacitor, the other end of the boosting capacitor is grounded, and a first current limiting resistor is connected with the boosting capacitor in parallel; the boosting power supply is accessed to a CPU (Central Processing Unit) through a first analog input interface; a launching control power supply is connected to the boosting power supply through a second current limiting resistor and a double-pole and double-throw relay which is connected with a resistance measuring pathway, and a switch of the relay is connected with a firing circuit of a controlled rocket; the resistance measuring pathway is accessed to the CPU through a second analog input interface; the control end of the relay is accessed to the CPU through a DI/DO (Digital Input/Digital Output) interface; a control instruction output from outside is received by the CPU and is transmitted to the control end of a launc</description><subject>APPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS,e.g. CANNONS</subject><subject>BLASTING</subject><subject>HARPOON GUNS</subject><subject>HEATING</subject><subject>LAUNCHERS FOR ROCKETS OR TORPEDOES</subject><subject>LIGHTING</subject><subject>MECHANICAL ENGINEERING</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2016</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZJAPyk_OTi1RyEkszUvOyMxLV0jOzyspys9RKK4sLknN5WFgTUvMKU7lhdLcDIpuriHOHrqpBfnxqcUFicmpeakl8c5-hgamJiYmZoYWjsbEqAEAQyQlLw</recordid><startdate>20160330</startdate><enddate>20160330</enddate><creator>ZHENG BOHUA</creator><creator>SUN YONGTAO</creator><creator>JIN LYUSHENG</creator><creator>QIAO HONGXIA</creator><creator>CHENG TAO</creator><creator>LI HUIFANG</creator><creator>ZHANG XIAOHANG</creator><creator>LI JIAN</creator><creator>WEI XUHUI</creator><creator>ZHANG BAOCHUN</creator><creator>WANG XIAOXIA</creator><creator>GAN LU</creator><creator>LI LING</creator><creator>ZHU SIHUA</creator><creator>FAN YANPING</creator><creator>LIU XIAO</creator><creator>JIA XIADONG</creator><creator>GUO HUA</creator><creator>GU KANGLE</creator><creator>HANG JIA</creator><scope>EVB</scope></search><sort><creationdate>20160330</creationdate><title>Rocket launching control system</title><author>ZHENG BOHUA ; SUN YONGTAO ; JIN LYUSHENG ; QIAO HONGXIA ; CHENG TAO ; LI HUIFANG ; ZHANG XIAOHANG ; LI JIAN ; WEI XUHUI ; ZHANG BAOCHUN ; WANG XIAOXIA ; GAN LU ; LI LING ; ZHU SIHUA ; FAN YANPING ; LIU XIAO ; JIA XIADONG ; GUO HUA ; GU KANGLE ; HANG JIA</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_CN105444618A3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>chi ; eng</language><creationdate>2016</creationdate><topic>APPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS,e.g. CANNONS</topic><topic>BLASTING</topic><topic>HARPOON GUNS</topic><topic>HEATING</topic><topic>LAUNCHERS FOR ROCKETS OR TORPEDOES</topic><topic>LIGHTING</topic><topic>MECHANICAL ENGINEERING</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>ZHENG BOHUA</creatorcontrib><creatorcontrib>SUN YONGTAO</creatorcontrib><creatorcontrib>JIN LYUSHENG</creatorcontrib><creatorcontrib>QIAO HONGXIA</creatorcontrib><creatorcontrib>CHENG TAO</creatorcontrib><creatorcontrib>LI HUIFANG</creatorcontrib><creatorcontrib>ZHANG XIAOHANG</creatorcontrib><creatorcontrib>LI JIAN</creatorcontrib><creatorcontrib>WEI XUHUI</creatorcontrib><creatorcontrib>ZHANG BAOCHUN</creatorcontrib><creatorcontrib>WANG XIAOXIA</creatorcontrib><creatorcontrib>GAN LU</creatorcontrib><creatorcontrib>LI LING</creatorcontrib><creatorcontrib>ZHU SIHUA</creatorcontrib><creatorcontrib>FAN YANPING</creatorcontrib><creatorcontrib>LIU XIAO</creatorcontrib><creatorcontrib>JIA XIADONG</creatorcontrib><creatorcontrib>GUO HUA</creatorcontrib><creatorcontrib>GU KANGLE</creatorcontrib><creatorcontrib>HANG JIA</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>ZHENG BOHUA</au><au>SUN YONGTAO</au><au>JIN LYUSHENG</au><au>QIAO HONGXIA</au><au>CHENG TAO</au><au>LI HUIFANG</au><au>ZHANG XIAOHANG</au><au>LI JIAN</au><au>WEI XUHUI</au><au>ZHANG BAOCHUN</au><au>WANG XIAOXIA</au><au>GAN LU</au><au>LI LING</au><au>ZHU SIHUA</au><au>FAN YANPING</au><au>LIU XIAO</au><au>JIA XIADONG</au><au>GUO HUA</au><au>GU KANGLE</au><au>HANG JIA</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Rocket launching control system</title><date>2016-03-30</date><risdate>2016</risdate><abstract>The invention discloses a rocket launching control system. Specifically, a boosting power supply is connected to one end of a boosting capacitor, the other end of the boosting capacitor is grounded, and a first current limiting resistor is connected with the boosting capacitor in parallel; the boosting power supply is accessed to a CPU (Central Processing Unit) through a first analog input interface; a launching control power supply is connected to the boosting power supply through a second current limiting resistor and a double-pole and double-throw relay which is connected with a resistance measuring pathway, and a switch of the relay is connected with a firing circuit of a controlled rocket; the resistance measuring pathway is accessed to the CPU through a second analog input interface; the control end of the relay is accessed to the CPU through a DI/DO (Digital Input/Digital Output) interface; a control instruction output from outside is received by the CPU and is transmitted to the control end of a launc</abstract><oa>free_for_read</oa></addata></record> |
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| language | chi ; eng |
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| subjects | APPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS,e.g. CANNONS BLASTING HARPOON GUNS HEATING LAUNCHERS FOR ROCKETS OR TORPEDOES LIGHTING MECHANICAL ENGINEERING WEAPONS |
| title | Rocket launching control system |
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