MOTOR CONTROL DESIRED DYNAMIC LOAD OF A SIMULATING SYSTEM AND METHOD
An apparatus and method for simulating a desired response in accordance with an external applied force (Fin). The apparatus includes a member (30b) which is responsive to the applied force, an actuator (20) coupled to the member for exerting a torque on the member, a force sensor (32) for detecting...
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| creator | HART WILLIAM A TRANKLE THOMAS L NORRIS, III UPTON T EYERMANN ROGER E HILDRETH BRUCE L |
| description | An apparatus and method for simulating a desired response in accordance with an external applied force (Fin). The apparatus includes a member (30b) which is responsive to the applied force, an actuator (20) coupled to the member for exerting a torque on the member, a force sensor (32) for detecting the applied force (Fin), and a torque sensor (22) for detecting the troque exerted by the actuator (20). Signals from the force sensor are used to determine the system response based upon a desired relation. The force sensor signals also are used to determine the actual system response based upon the physical characteristics of the apparatus. The detected torque is compared with the desired and the actual system response, and as a result of the comparison the torque exerted by the actuator onto the member is adjusted accordingly so that the member performs the desired system response. The actuator (20) is preferably an electric motor so that the apparatus can simulate any desired response, notwithstanding the physical characteristics of the system. |
| format | Patent |
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The apparatus includes a member (30b) which is responsive to the applied force, an actuator (20) coupled to the member for exerting a torque on the member, a force sensor (32) for detecting the applied force (Fin), and a torque sensor (22) for detecting the troque exerted by the actuator (20). Signals from the force sensor are used to determine the system response based upon a desired relation. The force sensor signals also are used to determine the actual system response based upon the physical characteristics of the apparatus. The detected torque is compared with the desired and the actual system response, and as a result of the comparison the torque exerted by the actuator onto the member is adjusted accordingly so that the member performs the desired system response. The actuator (20) is preferably an electric motor so that the apparatus can simulate any desired response, notwithstanding the physical characteristics of the system.</description><language>eng</language><subject>ADVERTISING ; AEROPLANES ; AIRCRAFT ; APPLIANCES FOR TEACHING, OR COMMUNICATING WITH, THE BLIND,DEAF OR MUTE ; AVIATION ; CONTROL DEVICES OR SYSTEMS INSOFAR AS CHARACTERISED BYMECHANICAL FEATURES ONLY ; CONTROL OR REGULATION OF ELECTRIC MOTORS, ELECTRIC GENERATORSOR DYNAMO-ELECTRIC CONVERTERS ; CONTROLLING ; CONTROLLING TRANSFORMERS, REACTORS OR CHOKE COILS ; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER ; COSMONAUTICS ; CRYPTOGRAPHY ; DIAGRAMS ; DISPLAY ; EDUCATION ; EDUCATIONAL OR DEMONSTRATION APPLIANCES ; ELECTRICITY ; GENERATION ; GLOBES ; HELICOPTERS ; PERFORMING OPERATIONS ; PHYSICS ; PLANETARIA ; REGULATING ; SEALS ; SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES ; TRANSPORTING</subject><creationdate>1993</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=19930511&DB=EPODOC&CC=US&NR=5209661A$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25542,76289</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=19930511&DB=EPODOC&CC=US&NR=5209661A$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>HART; WILLIAM A</creatorcontrib><creatorcontrib>TRANKLE; THOMAS L</creatorcontrib><creatorcontrib>NORRIS, III; UPTON T</creatorcontrib><creatorcontrib>EYERMANN; ROGER E</creatorcontrib><creatorcontrib>HILDRETH; BRUCE L</creatorcontrib><title>MOTOR CONTROL DESIRED DYNAMIC LOAD OF A SIMULATING SYSTEM AND METHOD</title><description>An apparatus and method for simulating a desired response in accordance with an external applied force (Fin). The apparatus includes a member (30b) which is responsive to the applied force, an actuator (20) coupled to the member for exerting a torque on the member, a force sensor (32) for detecting the applied force (Fin), and a torque sensor (22) for detecting the troque exerted by the actuator (20). Signals from the force sensor are used to determine the system response based upon a desired relation. The force sensor signals also are used to determine the actual system response based upon the physical characteristics of the apparatus. The detected torque is compared with the desired and the actual system response, and as a result of the comparison the torque exerted by the actuator onto the member is adjusted accordingly so that the member performs the desired system response. The actuator (20) is preferably an electric motor so that the apparatus can simulate any desired response, notwithstanding the physical characteristics of the system.</description><subject>ADVERTISING</subject><subject>AEROPLANES</subject><subject>AIRCRAFT</subject><subject>APPLIANCES FOR TEACHING, OR COMMUNICATING WITH, THE BLIND,DEAF OR MUTE</subject><subject>AVIATION</subject><subject>CONTROL DEVICES OR SYSTEMS INSOFAR AS CHARACTERISED BYMECHANICAL FEATURES ONLY</subject><subject>CONTROL OR REGULATION OF ELECTRIC MOTORS, ELECTRIC GENERATORSOR DYNAMO-ELECTRIC CONVERTERS</subject><subject>CONTROLLING</subject><subject>CONTROLLING TRANSFORMERS, REACTORS OR CHOKE COILS</subject><subject>CONVERSION OR DISTRIBUTION OF ELECTRIC POWER</subject><subject>COSMONAUTICS</subject><subject>CRYPTOGRAPHY</subject><subject>DIAGRAMS</subject><subject>DISPLAY</subject><subject>EDUCATION</subject><subject>EDUCATIONAL OR DEMONSTRATION APPLIANCES</subject><subject>ELECTRICITY</subject><subject>GENERATION</subject><subject>GLOBES</subject><subject>HELICOPTERS</subject><subject>PERFORMING OPERATIONS</subject><subject>PHYSICS</subject><subject>PLANETARIA</subject><subject>REGULATING</subject><subject>SEALS</subject><subject>SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES</subject><subject>TRANSPORTING</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>1993</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZHDx9Q_xD1Jw9vcLCfL3UXBxDfYMcnVRcIn0c_T1dFbw8Xd0UfB3U3BUCPb0DfVxDPH0c1cIjgwOcfVVcPRzUfB1DfHwd-FhYE1LzClO5YXS3Azybq4hzh66qQX58anFBYnJqXmpJfGhwaZGBpZmZoaOxoRVAACi0Sry</recordid><startdate>19930511</startdate><enddate>19930511</enddate><creator>HART; WILLIAM A</creator><creator>TRANKLE; THOMAS L</creator><creator>NORRIS, III; UPTON T</creator><creator>EYERMANN; ROGER E</creator><creator>HILDRETH; BRUCE L</creator><scope>EVB</scope></search><sort><creationdate>19930511</creationdate><title>MOTOR CONTROL DESIRED DYNAMIC LOAD OF A SIMULATING SYSTEM AND METHOD</title><author>HART; WILLIAM A ; TRANKLE; THOMAS L ; NORRIS, III; UPTON T ; EYERMANN; ROGER E ; HILDRETH; BRUCE L</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_US5209661A3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng</language><creationdate>1993</creationdate><topic>ADVERTISING</topic><topic>AEROPLANES</topic><topic>AIRCRAFT</topic><topic>APPLIANCES FOR TEACHING, OR COMMUNICATING WITH, THE BLIND,DEAF OR MUTE</topic><topic>AVIATION</topic><topic>CONTROL DEVICES OR SYSTEMS INSOFAR AS CHARACTERISED BYMECHANICAL FEATURES ONLY</topic><topic>CONTROL OR REGULATION OF ELECTRIC MOTORS, ELECTRIC GENERATORSOR DYNAMO-ELECTRIC CONVERTERS</topic><topic>CONTROLLING</topic><topic>CONTROLLING TRANSFORMERS, REACTORS OR CHOKE COILS</topic><topic>CONVERSION OR DISTRIBUTION OF ELECTRIC POWER</topic><topic>COSMONAUTICS</topic><topic>CRYPTOGRAPHY</topic><topic>DIAGRAMS</topic><topic>DISPLAY</topic><topic>EDUCATION</topic><topic>EDUCATIONAL OR DEMONSTRATION APPLIANCES</topic><topic>ELECTRICITY</topic><topic>GENERATION</topic><topic>GLOBES</topic><topic>HELICOPTERS</topic><topic>PERFORMING OPERATIONS</topic><topic>PHYSICS</topic><topic>PLANETARIA</topic><topic>REGULATING</topic><topic>SEALS</topic><topic>SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES</topic><topic>TRANSPORTING</topic><toplevel>online_resources</toplevel><creatorcontrib>HART; WILLIAM A</creatorcontrib><creatorcontrib>TRANKLE; THOMAS L</creatorcontrib><creatorcontrib>NORRIS, III; UPTON T</creatorcontrib><creatorcontrib>EYERMANN; ROGER E</creatorcontrib><creatorcontrib>HILDRETH; BRUCE L</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>HART; WILLIAM A</au><au>TRANKLE; THOMAS L</au><au>NORRIS, III; UPTON T</au><au>EYERMANN; ROGER E</au><au>HILDRETH; BRUCE L</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>MOTOR CONTROL DESIRED DYNAMIC LOAD OF A SIMULATING SYSTEM AND METHOD</title><date>1993-05-11</date><risdate>1993</risdate><abstract>An apparatus and method for simulating a desired response in accordance with an external applied force (Fin). The apparatus includes a member (30b) which is responsive to the applied force, an actuator (20) coupled to the member for exerting a torque on the member, a force sensor (32) for detecting the applied force (Fin), and a torque sensor (22) for detecting the troque exerted by the actuator (20). Signals from the force sensor are used to determine the system response based upon a desired relation. The force sensor signals also are used to determine the actual system response based upon the physical characteristics of the apparatus. The detected torque is compared with the desired and the actual system response, and as a result of the comparison the torque exerted by the actuator onto the member is adjusted accordingly so that the member performs the desired system response. The actuator (20) is preferably an electric motor so that the apparatus can simulate any desired response, notwithstanding the physical characteristics of the system.</abstract><oa>free_for_read</oa></addata></record> |
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| subjects | ADVERTISING AEROPLANES AIRCRAFT APPLIANCES FOR TEACHING, OR COMMUNICATING WITH, THE BLIND,DEAF OR MUTE AVIATION CONTROL DEVICES OR SYSTEMS INSOFAR AS CHARACTERISED BYMECHANICAL FEATURES ONLY CONTROL OR REGULATION OF ELECTRIC MOTORS, ELECTRIC GENERATORSOR DYNAMO-ELECTRIC CONVERTERS CONTROLLING CONTROLLING TRANSFORMERS, REACTORS OR CHOKE COILS CONVERSION OR DISTRIBUTION OF ELECTRIC POWER COSMONAUTICS CRYPTOGRAPHY DIAGRAMS DISPLAY EDUCATION EDUCATIONAL OR DEMONSTRATION APPLIANCES ELECTRICITY GENERATION GLOBES HELICOPTERS PERFORMING OPERATIONS PHYSICS PLANETARIA REGULATING SEALS SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES TRANSPORTING |
| title | MOTOR CONTROL DESIRED DYNAMIC LOAD OF A SIMULATING SYSTEM AND METHOD |
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