METHOD FOR MONITORING THE EXECUTION OF A GRAPHICAL CALCULATION AND DISPLAY CHAIN ASSOCIATED WITH AN AIRCRAFT COCKPIT DISPLAY SCREEN
The invention relates to this method comprising the following steps, for at least one input/output parameter:duplicating and inserting a list of graphical commands associated with said parameter within a calculation module of said chain,from a current value of said parameter, obtaining a current cyc...
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| creator | CHABOT, Philippe |
| description | The invention relates to this method comprising the following steps, for at least one input/output parameter:duplicating and inserting a list of graphical commands associated with said parameter within a calculation module of said chain,from a current value of said parameter, obtaining a current cyclic redundancy code associated with a current micropattern, generated by executing said at least one list,comparing said current cyclic redundancy code with a reference cyclic redundancy code stored in a dedicated memory space for a substantially identical value of said parameter within a tolerance threshold,in the event of a difference in cyclic redundancy code value, automatic sanctioning of said chain at least by suspending its execution. |
| format | Patent |
| fullrecord | <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_US2022223078A1</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>US2022223078A1</sourcerecordid><originalsourceid>FETCH-epo_espacenet_US2022223078A13</originalsourceid><addsrcrecordid>eNqNi7EKwkAQRNNYiPoPC9ZCTAptl81dbjG5C3cb1CoEOSvRQPwDf9wgYu3AMDDzZp68aiXGFaCdh9pZFufZliBGgTopaoWdBacBofTYGCasYDK1FX4mtAUUHJoKz0AGeWpCcMQoqoAji5kIQPbkUQuQo0PD8nsE8krZZTK79rcxrr65SNZaCZlNHB5dHIf-Eu_x2bUhS7NJebrb4zb_j3oD4UQ9jw</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>METHOD FOR MONITORING THE EXECUTION OF A GRAPHICAL CALCULATION AND DISPLAY CHAIN ASSOCIATED WITH AN AIRCRAFT COCKPIT DISPLAY SCREEN</title><source>esp@cenet</source><creator>CHABOT, Philippe</creator><creatorcontrib>CHABOT, Philippe</creatorcontrib><description>The invention relates to this method comprising the following steps, for at least one input/output parameter:duplicating and inserting a list of graphical commands associated with said parameter within a calculation module of said chain,from a current value of said parameter, obtaining a current cyclic redundancy code associated with a current micropattern, generated by executing said at least one list,comparing said current cyclic redundancy code with a reference cyclic redundancy code stored in a dedicated memory space for a substantially identical value of said parameter within a tolerance threshold,in the event of a difference in cyclic redundancy code value, automatic sanctioning of said chain at least by suspending its execution.</description><language>eng</language><subject>ADVERTISING ; AIRCRAFT ; ARRANGEMENTS OR CIRCUITS FOR CONTROL OF INDICATING DEVICESUSING STATIC MEANS TO PRESENT VARIABLE INFORMATION ; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT ; AVIATION ; CALCULATING ; COMPUTING ; COSMONAUTICS ; COUNTING ; CRYPTOGRAPHY ; DISPLAY ; EDUCATION ; EQUIPMENT FOR FITTING IN OR TO AIRCRAFT ; FLYING SUITS ; IMAGE DATA PROCESSING OR GENERATION, IN GENERAL ; PARACHUTES ; PERFORMING OPERATIONS ; PHYSICS ; SEALS ; 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relates to this method comprising the following steps, for at least one input/output parameter:duplicating and inserting a list of graphical commands associated with said parameter within a calculation module of said chain,from a current value of said parameter, obtaining a current cyclic redundancy code associated with a current micropattern, generated by executing said at least one list,comparing said current cyclic redundancy code with a reference cyclic redundancy code stored in a dedicated memory space for a substantially identical value of said parameter within a tolerance threshold,in the event of a difference in cyclic redundancy code value, automatic sanctioning of said chain at least by suspending its execution.</description><subject>ADVERTISING</subject><subject>AIRCRAFT</subject><subject>ARRANGEMENTS OR CIRCUITS FOR CONTROL OF INDICATING DEVICESUSING STATIC MEANS TO PRESENT VARIABLE INFORMATION</subject><subject>ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT</subject><subject>AVIATION</subject><subject>CALCULATING</subject><subject>COMPUTING</subject><subject>COSMONAUTICS</subject><subject>COUNTING</subject><subject>CRYPTOGRAPHY</subject><subject>DISPLAY</subject><subject>EDUCATION</subject><subject>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</subject><subject>FLYING SUITS</subject><subject>IMAGE DATA PROCESSING OR GENERATION, IN GENERAL</subject><subject>PARACHUTES</subject><subject>PERFORMING OPERATIONS</subject><subject>PHYSICS</subject><subject>SEALS</subject><subject>TRANSPORTING</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2022</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNqNi7EKwkAQRNNYiPoPC9ZCTAptl81dbjG5C3cb1CoEOSvRQPwDf9wgYu3AMDDzZp68aiXGFaCdh9pZFufZliBGgTopaoWdBacBofTYGCasYDK1FX4mtAUUHJoKz0AGeWpCcMQoqoAji5kIQPbkUQuQo0PD8nsE8krZZTK79rcxrr65SNZaCZlNHB5dHIf-Eu_x2bUhS7NJebrb4zb_j3oD4UQ9jw</recordid><startdate>20220714</startdate><enddate>20220714</enddate><creator>CHABOT, Philippe</creator><scope>EVB</scope></search><sort><creationdate>20220714</creationdate><title>METHOD FOR MONITORING THE EXECUTION OF A GRAPHICAL CALCULATION AND DISPLAY CHAIN ASSOCIATED WITH AN AIRCRAFT COCKPIT DISPLAY SCREEN</title><author>CHABOT, Philippe</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_US2022223078A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng</language><creationdate>2022</creationdate><topic>ADVERTISING</topic><topic>AIRCRAFT</topic><topic>ARRANGEMENTS OR CIRCUITS FOR CONTROL OF INDICATING DEVICESUSING STATIC MEANS TO PRESENT VARIABLE INFORMATION</topic><topic>ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT</topic><topic>AVIATION</topic><topic>CALCULATING</topic><topic>COMPUTING</topic><topic>COSMONAUTICS</topic><topic>COUNTING</topic><topic>CRYPTOGRAPHY</topic><topic>DISPLAY</topic><topic>EDUCATION</topic><topic>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</topic><topic>FLYING SUITS</topic><topic>IMAGE DATA PROCESSING OR GENERATION, IN GENERAL</topic><topic>PARACHUTES</topic><topic>PERFORMING OPERATIONS</topic><topic>PHYSICS</topic><topic>SEALS</topic><topic>TRANSPORTING</topic><toplevel>online_resources</toplevel><creatorcontrib>CHABOT, Philippe</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>CHABOT, Philippe</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>METHOD FOR MONITORING THE EXECUTION OF A GRAPHICAL CALCULATION AND DISPLAY CHAIN ASSOCIATED WITH AN AIRCRAFT COCKPIT DISPLAY SCREEN</title><date>2022-07-14</date><risdate>2022</risdate><abstract>The invention relates to this method comprising the following steps, for at least one input/output parameter:duplicating and inserting a list of graphical commands associated with said parameter within a calculation module of said chain,from a current value of said parameter, obtaining a current cyclic redundancy code associated with a current micropattern, generated by executing said at least one list,comparing said current cyclic redundancy code with a reference cyclic redundancy code stored in a dedicated memory space for a substantially identical value of said parameter within a tolerance threshold,in the event of a difference in cyclic redundancy code value, automatic sanctioning of said chain at least by suspending its execution.</abstract><oa>free_for_read</oa></addata></record> |
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| subjects | ADVERTISING AIRCRAFT ARRANGEMENTS OR CIRCUITS FOR CONTROL OF INDICATING DEVICESUSING STATIC MEANS TO PRESENT VARIABLE INFORMATION ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION CALCULATING COMPUTING COSMONAUTICS COUNTING CRYPTOGRAPHY DISPLAY EDUCATION EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS IMAGE DATA PROCESSING OR GENERATION, IN GENERAL PARACHUTES PERFORMING OPERATIONS PHYSICS SEALS TRANSPORTING |
| title | METHOD FOR MONITORING THE EXECUTION OF A GRAPHICAL CALCULATION AND DISPLAY CHAIN ASSOCIATED WITH AN AIRCRAFT COCKPIT DISPLAY SCREEN |
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