METHODS AND APPARATUSES FOR AUTONOMOUS FLIGHT TERMINATION
Embodiments include a flight safety assembly onboard an aerial vehicle, which includes a first sensor configured to sense first information related to flight of the aerial vehicle and a second sensor configured to sense second information related to the flight of the aerial vehicle. A sensor input i...
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| creator | DEVRIES DEREK R THOMAS STEVEN W DEDON CHARLES L VAN DIXHORN TIMOTHY J WEIGEL CHARLES L PAPADOPOULOS GEORGE B |
| description | Embodiments include a flight safety assembly onboard an aerial vehicle, which includes a first sensor configured to sense first information related to flight of the aerial vehicle and a second sensor configured to sense second information related to the flight of the aerial vehicle. A sensor input is adapted to receive third information related to the flight of the aerial vehicle. A processor is operably coupled to the first sensor, the second sensor, and the sensor input. The processor is configured to determine three independent instantaneous impact points for the aerial vehicle by independently analyzing each of the first information, the second information and the third information. The processor is also configured to generate three independent onboard flight termination indicators for each of the three independent instantaneous impact points that intersects with a region to be protected. |
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The processor is also configured to generate three independent onboard flight termination indicators for each of the three independent instantaneous impact points that intersects with a region to be protected.</description><subject>AMMUNITION</subject><subject>BLASTING</subject><subject>EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION</subject><subject>HEATING</subject><subject>LIGHTING</subject><subject>MECHANICAL ENGINEERING</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2014</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZLD0dQ3x8HcJVnD0c1FwDAhwDHIMCQ12DVZw8w9ScAwN8ffz9_UPBXJ9PN09QhRCXIN8Pf0cQzz9_XgYWNMSc4pTeaE0N4Oym2uIs4duakF-fGpxQWJyal5qSXxosJGBoYmBmbmhmYmjoTFxqgBW0CoL</recordid><startdate>20140306</startdate><enddate>20140306</enddate><creator>DEVRIES DEREK R</creator><creator>THOMAS STEVEN W</creator><creator>DEDON CHARLES L</creator><creator>VAN DIXHORN TIMOTHY J</creator><creator>WEIGEL CHARLES L</creator><creator>PAPADOPOULOS GEORGE B</creator><scope>EVB</scope></search><sort><creationdate>20140306</creationdate><title>METHODS AND APPARATUSES FOR AUTONOMOUS FLIGHT TERMINATION</title><author>DEVRIES DEREK R ; THOMAS STEVEN W ; DEDON CHARLES L ; VAN DIXHORN TIMOTHY J ; WEIGEL CHARLES L ; PAPADOPOULOS GEORGE B</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_US2014067164A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng</language><creationdate>2014</creationdate><topic>AMMUNITION</topic><topic>BLASTING</topic><topic>EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION</topic><topic>HEATING</topic><topic>LIGHTING</topic><topic>MECHANICAL ENGINEERING</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>DEVRIES DEREK R</creatorcontrib><creatorcontrib>THOMAS STEVEN W</creatorcontrib><creatorcontrib>DEDON CHARLES L</creatorcontrib><creatorcontrib>VAN DIXHORN TIMOTHY J</creatorcontrib><creatorcontrib>WEIGEL CHARLES L</creatorcontrib><creatorcontrib>PAPADOPOULOS GEORGE B</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>DEVRIES DEREK R</au><au>THOMAS STEVEN W</au><au>DEDON CHARLES L</au><au>VAN DIXHORN TIMOTHY J</au><au>WEIGEL CHARLES L</au><au>PAPADOPOULOS GEORGE B</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>METHODS AND APPARATUSES FOR AUTONOMOUS FLIGHT TERMINATION</title><date>2014-03-06</date><risdate>2014</risdate><abstract>Embodiments include a flight safety assembly onboard an aerial vehicle, which includes a first sensor configured to sense first information related to flight of the aerial vehicle and a second sensor configured to sense second information related to the flight of the aerial vehicle. A sensor input is adapted to receive third information related to the flight of the aerial vehicle. A processor is operably coupled to the first sensor, the second sensor, and the sensor input. The processor is configured to determine three independent instantaneous impact points for the aerial vehicle by independently analyzing each of the first information, the second information and the third information. The processor is also configured to generate three independent onboard flight termination indicators for each of the three independent instantaneous impact points that intersects with a region to be protected.</abstract><oa>free_for_read</oa></addata></record> |
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| subjects | AMMUNITION BLASTING EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION HEATING LIGHTING MECHANICAL ENGINEERING WEAPONS |
| title | METHODS AND APPARATUSES FOR AUTONOMOUS FLIGHT TERMINATION |
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