Full-trajectory intelligent collaborative planning launching method for unpowered guided projectile, electronic equipment and storage medium
The invention discloses a full-ballistic intelligent collaborative planning launching method for an unpowered guided projectile, electronic equipment and a storage medium, belongs to the field of automatic control, and aims to solve the problem of full-ballistic intelligent collaborative planning la...
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| creator | JIANG SHANG MA YE CAI CHANG ZHANG GANG XIE WEIHE PANG WEI |
| description | The invention discloses a full-ballistic intelligent collaborative planning launching method for an unpowered guided projectile, electronic equipment and a storage medium, belongs to the field of automatic control, and aims to solve the problem of full-ballistic intelligent collaborative planning launching of the unpowered guided projectile without continuous controllable power and with limited control allowance. Comprising the steps that according to a target function, the flight time difference of any two adjacent guided projectiles reaching the tail-section designated airspace and the sum of the flight time of all the projectiles are obtained; determining a middle section planning trajectory of the guided projectile according to the optimal group of middle section trajectory parameters; a steering engine control instruction is generated according to the parameter deviation between the middle-section actual ballistic trajectories of the guided projectiles and the middle-section planned ballistic trajectorie |
| format | Patent |
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Comprising the steps that according to a target function, the flight time difference of any two adjacent guided projectiles reaching the tail-section designated airspace and the sum of the flight time of all the projectiles are obtained; determining a middle section planning trajectory of the guided projectile according to the optimal group of middle section trajectory parameters; a steering engine control instruction is generated according to the parameter deviation between the middle-section actual ballistic trajectories of the guided projectiles and the middle-section planned ballistic trajectorie</description><language>chi ; eng</language><subject>AMMUNITION ; APPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS,e.g. CANNONS ; BLASTING ; CALCULATING ; COMPUTING ; COUNTING ; ELECTRIC DIGITAL DATA PROCESSING ; EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION ; HARPOON GUNS ; HEATING ; LAUNCHERS FOR ROCKETS OR TORPEDOES ; LIGHTING ; MECHANICAL ENGINEERING ; PHYSICS ; WEAPONS</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=20230704&DB=EPODOC&CC=CN&NR=116379836A$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25542,76289</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20230704&DB=EPODOC&CC=CN&NR=116379836A$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>JIANG SHANG</creatorcontrib><creatorcontrib>MA YE</creatorcontrib><creatorcontrib>CAI CHANG</creatorcontrib><creatorcontrib>ZHANG GANG</creatorcontrib><creatorcontrib>XIE WEIHE</creatorcontrib><creatorcontrib>PANG WEI</creatorcontrib><title>Full-trajectory intelligent collaborative planning launching method for unpowered guided projectile, electronic equipment and storage medium</title><description>The invention discloses a full-ballistic intelligent collaborative planning launching method for an unpowered guided projectile, electronic equipment and a storage medium, belongs to the field of automatic control, and aims to solve the problem of full-ballistic intelligent collaborative planning launching of the unpowered guided projectile without continuous controllable power and with limited control allowance. Comprising the steps that according to a target function, the flight time difference of any two adjacent guided projectiles reaching the tail-section designated airspace and the sum of the flight time of all the projectiles are obtained; determining a middle section planning trajectory of the guided projectile according to the optimal group of middle section trajectory parameters; a steering engine control instruction is generated according to the parameter deviation between the middle-section actual ballistic trajectories of the guided projectiles and the middle-section planned ballistic trajectorie</description><subject>AMMUNITION</subject><subject>APPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS,e.g. CANNONS</subject><subject>BLASTING</subject><subject>CALCULATING</subject><subject>COMPUTING</subject><subject>COUNTING</subject><subject>ELECTRIC DIGITAL DATA PROCESSING</subject><subject>EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION</subject><subject>HARPOON GUNS</subject><subject>HEATING</subject><subject>LAUNCHERS FOR ROCKETS OR TORPEDOES</subject><subject>LIGHTING</subject><subject>MECHANICAL ENGINEERING</subject><subject>PHYSICS</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2023</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNqNjTsOwkAMBdNQIOAOpocCReJTIgSioqJHZtckRo69bHZB3IFDk0gcgGqmeJo3LD6HLDJPEe_kksU3sCYS4Yo0gTMRvFrExE-CIKjKWoFgVlf31lCqzcPNImQN9qJIHqrMvkOI1jdZaAYknUVTdkCPzKHp66ge2u4TK-pCnnMzLgY3lJYmP46K6WF_3h3nFOxCbUBHSumyOy0Wy3K1WZfLbfnP5gtNJk-B</recordid><startdate>20230704</startdate><enddate>20230704</enddate><creator>JIANG SHANG</creator><creator>MA YE</creator><creator>CAI CHANG</creator><creator>ZHANG GANG</creator><creator>XIE WEIHE</creator><creator>PANG WEI</creator><scope>EVB</scope></search><sort><creationdate>20230704</creationdate><title>Full-trajectory intelligent collaborative planning launching method for unpowered guided projectile, electronic equipment and storage medium</title><author>JIANG SHANG ; MA YE ; CAI CHANG ; ZHANG GANG ; XIE WEIHE ; PANG WEI</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_CN116379836A3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>chi ; eng</language><creationdate>2023</creationdate><topic>AMMUNITION</topic><topic>APPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS,e.g. CANNONS</topic><topic>BLASTING</topic><topic>CALCULATING</topic><topic>COMPUTING</topic><topic>COUNTING</topic><topic>ELECTRIC DIGITAL DATA PROCESSING</topic><topic>EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION</topic><topic>HARPOON GUNS</topic><topic>HEATING</topic><topic>LAUNCHERS FOR ROCKETS OR TORPEDOES</topic><topic>LIGHTING</topic><topic>MECHANICAL ENGINEERING</topic><topic>PHYSICS</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>JIANG SHANG</creatorcontrib><creatorcontrib>MA YE</creatorcontrib><creatorcontrib>CAI CHANG</creatorcontrib><creatorcontrib>ZHANG GANG</creatorcontrib><creatorcontrib>XIE WEIHE</creatorcontrib><creatorcontrib>PANG WEI</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>JIANG SHANG</au><au>MA YE</au><au>CAI CHANG</au><au>ZHANG GANG</au><au>XIE WEIHE</au><au>PANG WEI</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Full-trajectory intelligent collaborative planning launching method for unpowered guided projectile, electronic equipment and storage medium</title><date>2023-07-04</date><risdate>2023</risdate><abstract>The invention discloses a full-ballistic intelligent collaborative planning launching method for an unpowered guided projectile, electronic equipment and a storage medium, belongs to the field of automatic control, and aims to solve the problem of full-ballistic intelligent collaborative planning launching of the unpowered guided projectile without continuous controllable power and with limited control allowance. Comprising the steps that according to a target function, the flight time difference of any two adjacent guided projectiles reaching the tail-section designated airspace and the sum of the flight time of all the projectiles are obtained; determining a middle section planning trajectory of the guided projectile according to the optimal group of middle section trajectory parameters; a steering engine control instruction is generated according to the parameter deviation between the middle-section actual ballistic trajectories of the guided projectiles and the middle-section planned ballistic trajectorie</abstract><oa>free_for_read</oa></addata></record> |
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| subjects | AMMUNITION APPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS,e.g. CANNONS BLASTING CALCULATING COMPUTING COUNTING ELECTRIC DIGITAL DATA PROCESSING EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION HARPOON GUNS HEATING LAUNCHERS FOR ROCKETS OR TORPEDOES LIGHTING MECHANICAL ENGINEERING PHYSICS WEAPONS |
| title | Full-trajectory intelligent collaborative planning launching method for unpowered guided projectile, electronic equipment and storage medium |
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