SYSTEMS AND METHODS FOR PRODUCING TWO INDEPENDENT DISSIMILAR ATTITUDE SOLUTIONS, TWO INDEPENDENT DISSIMILAR INERTIAL SOLUTIONS OR BOTH FROM ONE IMPROVED NAVIGATION DEVICE
Systems and methods for producing two independent dissimilar attitude solutions, two independent dissimilar inertial solutions or both from one improved navigation device are disclosed. In one embodiment, an avionics system comprises: an inertial navigation device configured to produce a first set o...
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| creator | Miller Michael G Horner Adam Ross |
| description | Systems and methods for producing two independent dissimilar attitude solutions, two independent dissimilar inertial solutions or both from one improved navigation device are disclosed. In one embodiment, an avionics system comprises: an inertial navigation device configured to produce a first set of attitude solutions; an attitude heading and reference unit configured to produce a primary set of attitude solutions and a secondary set of attitude solutions; and a display device configured to receive the first set of attitude solutions, the primary set of attitude solutions and the secondary set of attitude solutions, wherein if the first set of attitude solutions and the primary set of attitude solutions are yielding different results, then the display device is configured to determine whether the first set of attitude solutions or the primary set of attitude solutions is correct by determining differences between the attitude solutions and determining which difference is below a threshold. |
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| fullrecord | <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_US2016273919A1</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>US2016273919A1</sourcerecordid><originalsourceid>FETCH-epo_espacenet_US2016273919A13</originalsourceid><addsrcrecordid>eNqNzTEKwkAQheE0FqLeYcBWwSgolmt2kgxkd2RnErESkbUSFeKpPKURBDuxea_54O8nT9mLohMw3oJDLdkK5BxgG9jWGfkCdMdA3uIWu_EKlkTIUWUCGFXS2iIIV7USe5n84uQxKJnqy6ErbVhLyAM7YI9Aris3aMGbhgrzVmCxoQyHSe98vLRx9PlBMs5Rs3Ia77dDbO_HU7zGx6GW-SxdzleLdbo26eI_9QL_ukmK</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>SYSTEMS AND METHODS FOR PRODUCING TWO INDEPENDENT DISSIMILAR ATTITUDE SOLUTIONS, TWO INDEPENDENT DISSIMILAR INERTIAL SOLUTIONS OR BOTH FROM ONE IMPROVED NAVIGATION DEVICE</title><source>esp@cenet</source><creator>Miller Michael G ; Horner Adam Ross</creator><creatorcontrib>Miller Michael G ; Horner Adam Ross</creatorcontrib><description>Systems and methods for producing two independent dissimilar attitude solutions, two independent dissimilar inertial solutions or both from one improved navigation device are disclosed. In one embodiment, an avionics system comprises: an inertial navigation device configured to produce a first set of attitude solutions; an attitude heading and reference unit configured to produce a primary set of attitude solutions and a secondary set of attitude solutions; and a display device configured to receive the first set of attitude solutions, the primary set of attitude solutions and the secondary set of attitude solutions, wherein if the first set of attitude solutions and the primary set of attitude solutions are yielding different results, then the display device is configured to determine whether the first set of attitude solutions or the primary set of attitude solutions is correct by determining differences between the attitude solutions and determining which difference is below a threshold.</description><language>eng</language><subject>ANALOGOUS ARRANGEMENTS USING OTHER WAVES ; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES ; GYROSCOPIC INSTRUMENTS ; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION ORRERADIATION OF RADIO WAVES ; MEASURING ; MEASURING DISTANCES, LEVELS OR BEARINGS ; NAVIGATION ; PHOTOGRAMMETRY OR VIDEOGRAMMETRY ; PHYSICS ; RADIO DIRECTION-FINDING ; RADIO NAVIGATION ; SURVEYING ; TESTING</subject><creationdate>2016</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=20160922&DB=EPODOC&CC=US&NR=2016273919A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20160922&DB=EPODOC&CC=US&NR=2016273919A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>Miller Michael G</creatorcontrib><creatorcontrib>Horner Adam Ross</creatorcontrib><title>SYSTEMS AND METHODS FOR PRODUCING TWO INDEPENDENT DISSIMILAR ATTITUDE SOLUTIONS, TWO INDEPENDENT DISSIMILAR INERTIAL SOLUTIONS OR BOTH FROM ONE IMPROVED NAVIGATION DEVICE</title><description>Systems and methods for producing two independent dissimilar attitude solutions, two independent dissimilar inertial solutions or both from one improved navigation device are disclosed. In one embodiment, an avionics system comprises: an inertial navigation device configured to produce a first set of attitude solutions; an attitude heading and reference unit configured to produce a primary set of attitude solutions and a secondary set of attitude solutions; and a display device configured to receive the first set of attitude solutions, the primary set of attitude solutions and the secondary set of attitude solutions, wherein if the first set of attitude solutions and the primary set of attitude solutions are yielding different results, then the display device is configured to determine whether the first set of attitude solutions or the primary set of attitude solutions is correct by determining differences between the attitude solutions and determining which difference is below a threshold.</description><subject>ANALOGOUS ARRANGEMENTS USING OTHER WAVES</subject><subject>DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES</subject><subject>GYROSCOPIC INSTRUMENTS</subject><subject>LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION ORRERADIATION OF RADIO WAVES</subject><subject>MEASURING</subject><subject>MEASURING DISTANCES, LEVELS OR BEARINGS</subject><subject>NAVIGATION</subject><subject>PHOTOGRAMMETRY OR VIDEOGRAMMETRY</subject><subject>PHYSICS</subject><subject>RADIO DIRECTION-FINDING</subject><subject>RADIO NAVIGATION</subject><subject>SURVEYING</subject><subject>TESTING</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2016</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNqNzTEKwkAQheE0FqLeYcBWwSgolmt2kgxkd2RnErESkbUSFeKpPKURBDuxea_54O8nT9mLohMw3oJDLdkK5BxgG9jWGfkCdMdA3uIWu_EKlkTIUWUCGFXS2iIIV7USe5n84uQxKJnqy6ErbVhLyAM7YI9Aris3aMGbhgrzVmCxoQyHSe98vLRx9PlBMs5Rs3Ia77dDbO_HU7zGx6GW-SxdzleLdbo26eI_9QL_ukmK</recordid><startdate>20160922</startdate><enddate>20160922</enddate><creator>Miller Michael G</creator><creator>Horner Adam Ross</creator><scope>EVB</scope></search><sort><creationdate>20160922</creationdate><title>SYSTEMS AND METHODS FOR PRODUCING TWO INDEPENDENT DISSIMILAR ATTITUDE SOLUTIONS, TWO INDEPENDENT DISSIMILAR INERTIAL SOLUTIONS OR BOTH FROM ONE IMPROVED NAVIGATION DEVICE</title><author>Miller Michael G ; Horner Adam Ross</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_US2016273919A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng</language><creationdate>2016</creationdate><topic>ANALOGOUS ARRANGEMENTS USING OTHER WAVES</topic><topic>DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES</topic><topic>GYROSCOPIC INSTRUMENTS</topic><topic>LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION ORRERADIATION OF RADIO WAVES</topic><topic>MEASURING</topic><topic>MEASURING DISTANCES, LEVELS OR BEARINGS</topic><topic>NAVIGATION</topic><topic>PHOTOGRAMMETRY OR VIDEOGRAMMETRY</topic><topic>PHYSICS</topic><topic>RADIO DIRECTION-FINDING</topic><topic>RADIO NAVIGATION</topic><topic>SURVEYING</topic><topic>TESTING</topic><toplevel>online_resources</toplevel><creatorcontrib>Miller Michael G</creatorcontrib><creatorcontrib>Horner Adam Ross</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Miller Michael G</au><au>Horner Adam Ross</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>SYSTEMS AND METHODS FOR PRODUCING TWO INDEPENDENT DISSIMILAR ATTITUDE SOLUTIONS, TWO INDEPENDENT DISSIMILAR INERTIAL SOLUTIONS OR BOTH FROM ONE IMPROVED NAVIGATION DEVICE</title><date>2016-09-22</date><risdate>2016</risdate><abstract>Systems and methods for producing two independent dissimilar attitude solutions, two independent dissimilar inertial solutions or both from one improved navigation device are disclosed. In one embodiment, an avionics system comprises: an inertial navigation device configured to produce a first set of attitude solutions; an attitude heading and reference unit configured to produce a primary set of attitude solutions and a secondary set of attitude solutions; and a display device configured to receive the first set of attitude solutions, the primary set of attitude solutions and the secondary set of attitude solutions, wherein if the first set of attitude solutions and the primary set of attitude solutions are yielding different results, then the display device is configured to determine whether the first set of attitude solutions or the primary set of attitude solutions is correct by determining differences between the attitude solutions and determining which difference is below a threshold.</abstract><oa>free_for_read</oa></addata></record> |
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| subjects | ANALOGOUS ARRANGEMENTS USING OTHER WAVES DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES GYROSCOPIC INSTRUMENTS LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION ORRERADIATION OF RADIO WAVES MEASURING MEASURING DISTANCES, LEVELS OR BEARINGS NAVIGATION PHOTOGRAMMETRY OR VIDEOGRAMMETRY PHYSICS RADIO DIRECTION-FINDING RADIO NAVIGATION SURVEYING TESTING |
| title | SYSTEMS AND METHODS FOR PRODUCING TWO INDEPENDENT DISSIMILAR ATTITUDE SOLUTIONS, TWO INDEPENDENT DISSIMILAR INERTIAL SOLUTIONS OR BOTH FROM ONE IMPROVED NAVIGATION DEVICE |
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