Method and apparatus for optimal guidance

A system for guiding a steerable object, such as a torpedo, from a launch site, such as a submarine, to a contact or target. The system generates two distinct sets of guidance commands. One set is based upon a guidance command model that is selected to be the optimal model for a given tactical situa...

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Hauptverfasser:	PINKOS, ROBERT F, BESSACINI, ANTHONY F
Format:	Patent
Sprache:	eng
Schlagworte:	AIMING BLASTING CONTROLLING HEATING LIGHTING MECHANICAL ENGINEERING PHYSICS REGULATING SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES WEAPON SIGHTS WEAPONS
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creator	PINKOS ROBERT F BESSACINI ANTHONY F
description	A system for guiding a steerable object, such as a torpedo, from a launch site, such as a submarine, to a contact or target. The system generates two distinct sets of guidance commands. One set is based upon a guidance command model that is selected to be the optimal model for a given tactical situation; the other, for a situation in which a communications path between the launch site and steerable object fails. At the steerable object, an integrity detector determines the integrity of the communications path. A command receptor and storage unit receives the two sets of signals corresponding to the two sets of selected commands. The one set is passed along so long as the communications path has integrity. Otherwise the system defaults and pursues guidance according to the second set of commands.
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One set is based upon a guidance command model that is selected to be the optimal model for a given tactical situation; the other, for a situation in which a communications path between the launch site and steerable object fails. At the steerable object, an integrity detector determines the integrity of the communications path. A command receptor and storage unit receives the two sets of signals corresponding to the two sets of selected commands. The one set is passed along so long as the communications path has integrity. Otherwise the system defaults and pursues guidance according to the second set of commands.</description><edition>6</edition><language>eng</language><subject>AIMING ; BLASTING ; CONTROLLING ; HEATING ; LIGHTING ; MECHANICAL ENGINEERING ; PHYSICS ; REGULATING ; SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES ; WEAPON SIGHTS ; WEAPONS</subject><creationdate>1997</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=19970610&DB=EPODOC&CC=US&NR=5637826A$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25542,76289</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=19970610&DB=EPODOC&CC=US&NR=5637826A$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>PINKOS; ROBERT F</creatorcontrib><creatorcontrib>BESSACINI; ANTHONY F</creatorcontrib><title>Method and apparatus for optimal guidance</title><description>A system for guiding a steerable object, such as a torpedo, from a launch site, such as a submarine, to a contact or target. The system generates two distinct sets of guidance commands. One set is based upon a guidance command model that is selected to be the optimal model for a given tactical situation; the other, for a situation in which a communications path between the launch site and steerable object fails. At the steerable object, an integrity detector determines the integrity of the communications path. A command receptor and storage unit receives the two sets of signals corresponding to the two sets of selected commands. The one set is passed along so long as the communications path has integrity. Otherwise the system defaults and pursues guidance according to the second set of commands.</description><subject>AIMING</subject><subject>BLASTING</subject><subject>CONTROLLING</subject><subject>HEATING</subject><subject>LIGHTING</subject><subject>MECHANICAL ENGINEERING</subject><subject>PHYSICS</subject><subject>REGULATING</subject><subject>SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES</subject><subject>WEAPON SIGHTS</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>1997</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZND0TS3JyE9RSMwD4oKCxKLEktJihbT8IoX8gpLM3MQchfTSzJTEvORUHgbWtMSc4lReKM3NIO_mGuLsoZtakB-fWlyQmJyal1oSHxpsamZsbmFk5mhMWAUAX3QoBg</recordid><startdate>19970610</startdate><enddate>19970610</enddate><creator>PINKOS; ROBERT F</creator><creator>BESSACINI; ANTHONY F</creator><scope>EVB</scope></search><sort><creationdate>19970610</creationdate><title>Method and apparatus for optimal guidance</title><author>PINKOS; ROBERT F ; BESSACINI; ANTHONY F</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_US5637826A3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng</language><creationdate>1997</creationdate><topic>AIMING</topic><topic>BLASTING</topic><topic>CONTROLLING</topic><topic>HEATING</topic><topic>LIGHTING</topic><topic>MECHANICAL ENGINEERING</topic><topic>PHYSICS</topic><topic>REGULATING</topic><topic>SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES</topic><topic>WEAPON SIGHTS</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>PINKOS; ROBERT F</creatorcontrib><creatorcontrib>BESSACINI; ANTHONY F</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>PINKOS; ROBERT F</au><au>BESSACINI; ANTHONY F</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Method and apparatus for optimal guidance</title><date>1997-06-10</date><risdate>1997</risdate><abstract>A system for guiding a steerable object, such as a torpedo, from a launch site, such as a submarine, to a contact or target. The system generates two distinct sets of guidance commands. One set is based upon a guidance command model that is selected to be the optimal model for a given tactical situation; the other, for a situation in which a communications path between the launch site and steerable object fails. At the steerable object, an integrity detector determines the integrity of the communications path. A command receptor and storage unit receives the two sets of signals corresponding to the two sets of selected commands. The one set is passed along so long as the communications path has integrity. Otherwise the system defaults and pursues guidance according to the second set of commands.</abstract><edition>6</edition><oa>free_for_read</oa></addata></record>
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subjects	AIMING BLASTING CONTROLLING HEATING LIGHTING MECHANICAL ENGINEERING PHYSICS REGULATING SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES WEAPON SIGHTS WEAPONS
title	Method and apparatus for optimal guidance
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