COLLISION AVOIDANCE FOR MANNED VERTICAL TAKE-OFF AND LANDING AERIAL VEHICLES
A manned vertical take-off and landing (VTOL) aerial vehicle comprises: a body comprising a cockpit having pilot-operable controls; a propulsion system carried by the body to propel the body during flight; a control system comprising a sensing system, a processor, and memory storing program instruct...
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| creator | BREUT, Florian PEARSON, Matthew James |
| description | A manned vertical take-off and landing (VTOL) aerial vehicle comprises: a body comprising a cockpit having pilot-operable controls; a propulsion system carried by the body to propel the body during flight; a control system comprising a sensing system, a processor, and memory storing program instructions configured to cause the processor to determine a state estimate of the aerial vehicle within a region, a repulsion vector based on a repulsion potential field model of the region and the state estimate, and a collision avoidance velocity vector based on the repulsion vector and the state estimate; determine an input vector indicative of an intended angular velocity and an intended thrust of the vehicle based on pilot-operable control inputs; determine a control vector based on the collision avoidance velocity vector and the input vector; and control the propulsion system such that the manned VTOL aerial vehicle avoids an object in the region. |
| format | Patent |
| fullrecord | <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_EP4268043A4</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>EP4268043A4</sourcerecordid><originalsourceid>FETCH-epo_espacenet_EP4268043A43</originalsourceid><addsrcrecordid>eNqNikEKwjAQAHPxIOof9gMFsUG8LsnGLq4bSUOupUg8iRbq_7EHH-Bl5jCzNuKiCPccFbBE9qiOIMQEV1QlD4VSZocCGS_UxBAA1YMsYD0DUuKlFerYCfVbs3qMz7nuft4YCJRd19TpPdR5Gu_1VT8D3ezheNrbFm37x_IFMJ0tHw</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>COLLISION AVOIDANCE FOR MANNED VERTICAL TAKE-OFF AND LANDING AERIAL VEHICLES</title><source>esp@cenet</source><creator>BREUT, Florian ; PEARSON, Matthew James</creator><creatorcontrib>BREUT, Florian ; PEARSON, Matthew James</creatorcontrib><description>A manned vertical take-off and landing (VTOL) aerial vehicle comprises: a body comprising a cockpit having pilot-operable controls; a propulsion system carried by the body to propel the body during flight; a control system comprising a sensing system, a processor, and memory storing program instructions configured to cause the processor to determine a state estimate of the aerial vehicle within a region, a repulsion vector based on a repulsion potential field model of the region and the state estimate, and a collision avoidance velocity vector based on the repulsion vector and the state estimate; determine an input vector indicative of an intended angular velocity and an intended thrust of the vehicle based on pilot-operable control inputs; determine a control vector based on the collision avoidance velocity vector and the input vector; and control the propulsion system such that the manned VTOL aerial vehicle avoids an object in the region.</description><language>eng ; fre ; ger</language><subject>AEROPLANES ; AIRCRAFT ; ANALOGOUS ARRANGEMENTS USING OTHER WAVES ; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT ; AVIATION ; CONTROLLING ; COSMONAUTICS ; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES ; EQUIPMENT FOR FITTING IN OR TO AIRCRAFT ; FLYING SUITS ; HELICOPTERS ; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION ORRERADIATION OF RADIO WAVES ; MEASURING ; PARACHUTES ; PERFORMING OPERATIONS ; PHYSICS ; RADIO DIRECTION-FINDING ; RADIO NAVIGATION ; REGULATING ; SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES ; TESTING ; TRANSPORTING</subject><creationdate>2024</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=20241106&DB=EPODOC&CC=EP&NR=4268043A4$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20241106&DB=EPODOC&CC=EP&NR=4268043A4$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>BREUT, Florian</creatorcontrib><creatorcontrib>PEARSON, Matthew James</creatorcontrib><title>COLLISION AVOIDANCE FOR MANNED VERTICAL TAKE-OFF AND LANDING AERIAL VEHICLES</title><description>A manned vertical take-off and landing (VTOL) aerial vehicle comprises: a body comprising a cockpit having pilot-operable controls; a propulsion system carried by the body to propel the body during flight; a control system comprising a sensing system, a processor, and memory storing program instructions configured to cause the processor to determine a state estimate of the aerial vehicle within a region, a repulsion vector based on a repulsion potential field model of the region and the state estimate, and a collision avoidance velocity vector based on the repulsion vector and the state estimate; determine an input vector indicative of an intended angular velocity and an intended thrust of the vehicle based on pilot-operable control inputs; determine a control vector based on the collision avoidance velocity vector and the input vector; and control the propulsion system such that the manned VTOL aerial vehicle avoids an object in the region.</description><subject>AEROPLANES</subject><subject>AIRCRAFT</subject><subject>ANALOGOUS ARRANGEMENTS USING OTHER WAVES</subject><subject>ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT</subject><subject>AVIATION</subject><subject>CONTROLLING</subject><subject>COSMONAUTICS</subject><subject>DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES</subject><subject>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</subject><subject>FLYING SUITS</subject><subject>HELICOPTERS</subject><subject>LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION ORRERADIATION OF RADIO WAVES</subject><subject>MEASURING</subject><subject>PARACHUTES</subject><subject>PERFORMING OPERATIONS</subject><subject>PHYSICS</subject><subject>RADIO DIRECTION-FINDING</subject><subject>RADIO NAVIGATION</subject><subject>REGULATING</subject><subject>SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES</subject><subject>TESTING</subject><subject>TRANSPORTING</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2024</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNqNikEKwjAQAHPxIOof9gMFsUG8LsnGLq4bSUOupUg8iRbq_7EHH-Bl5jCzNuKiCPccFbBE9qiOIMQEV1QlD4VSZocCGS_UxBAA1YMsYD0DUuKlFerYCfVbs3qMz7nuft4YCJRd19TpPdR5Gu_1VT8D3ezheNrbFm37x_IFMJ0tHw</recordid><startdate>20241106</startdate><enddate>20241106</enddate><creator>BREUT, Florian</creator><creator>PEARSON, Matthew James</creator><scope>EVB</scope></search><sort><creationdate>20241106</creationdate><title>COLLISION AVOIDANCE FOR MANNED VERTICAL TAKE-OFF AND LANDING AERIAL VEHICLES</title><author>BREUT, Florian ; PEARSON, Matthew James</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_EP4268043A43</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre ; ger</language><creationdate>2024</creationdate><topic>AEROPLANES</topic><topic>AIRCRAFT</topic><topic>ANALOGOUS ARRANGEMENTS USING OTHER WAVES</topic><topic>ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT</topic><topic>AVIATION</topic><topic>CONTROLLING</topic><topic>COSMONAUTICS</topic><topic>DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES</topic><topic>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</topic><topic>FLYING SUITS</topic><topic>HELICOPTERS</topic><topic>LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION ORRERADIATION OF RADIO WAVES</topic><topic>MEASURING</topic><topic>PARACHUTES</topic><topic>PERFORMING OPERATIONS</topic><topic>PHYSICS</topic><topic>RADIO DIRECTION-FINDING</topic><topic>RADIO NAVIGATION</topic><topic>REGULATING</topic><topic>SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES</topic><topic>TESTING</topic><topic>TRANSPORTING</topic><toplevel>online_resources</toplevel><creatorcontrib>BREUT, Florian</creatorcontrib><creatorcontrib>PEARSON, Matthew James</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>BREUT, Florian</au><au>PEARSON, Matthew James</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>COLLISION AVOIDANCE FOR MANNED VERTICAL TAKE-OFF AND LANDING AERIAL VEHICLES</title><date>2024-11-06</date><risdate>2024</risdate><abstract>A manned vertical take-off and landing (VTOL) aerial vehicle comprises: a body comprising a cockpit having pilot-operable controls; a propulsion system carried by the body to propel the body during flight; a control system comprising a sensing system, a processor, and memory storing program instructions configured to cause the processor to determine a state estimate of the aerial vehicle within a region, a repulsion vector based on a repulsion potential field model of the region and the state estimate, and a collision avoidance velocity vector based on the repulsion vector and the state estimate; determine an input vector indicative of an intended angular velocity and an intended thrust of the vehicle based on pilot-operable control inputs; determine a control vector based on the collision avoidance velocity vector and the input vector; and control the propulsion system such that the manned VTOL aerial vehicle avoids an object in the region.</abstract><oa>free_for_read</oa></addata></record> |
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| language | eng ; fre ; ger |
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| subjects | AEROPLANES AIRCRAFT ANALOGOUS ARRANGEMENTS USING OTHER WAVES ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION CONTROLLING COSMONAUTICS DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS HELICOPTERS LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION ORRERADIATION OF RADIO WAVES MEASURING PARACHUTES PERFORMING OPERATIONS PHYSICS RADIO DIRECTION-FINDING RADIO NAVIGATION REGULATING SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES TESTING TRANSPORTING |
| title | COLLISION AVOIDANCE FOR MANNED VERTICAL TAKE-OFF AND LANDING AERIAL VEHICLES |
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