http://rdf.ncbi.nlm.nih.gov/pubchem/patent/CN-115077516-A

Outgoing Links

Predicate Object
assignee http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_56e5f0cd8e364fbd0678338973e06077
classificationCPCInventive http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/G01C21-24
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/G01C21-165
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/H04W64-00
classificationIPCInventive http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/H04W64-00
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/G01C21-24
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/G01C21-16
filingDate 2022-02-11-04:00^^<http://www.w3.org/2001/XMLSchema#date>
inventor http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_177ecef375090a1d1d17784593fb4278
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_dcef2ecba4946721e6f3311d8603bfa8
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_2269837c5b8b51ebf9b1ef6ebafff52f
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_b81fe9dff4419fe081f189c3e09ce338
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_4dff6ff11bf8983447a989dd6253a543
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_59846bf3500ecb8ce017cad0afe86928
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_357cb8e320dccb021109600d83766be1
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_e80128b7ec536435ea440e7e8ac58471
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_14174981199512c192cff2b511d6fb33
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_6814bf2d7c9cd36bcd72cb15daff2853
publicationDate 2022-09-20-04:00^^<http://www.w3.org/2001/XMLSchema#date>
publicationNumber CN-115077516-A
titleOfInvention A method for acquiring attitude parameters of a vehicle before firing
abstract The present invention is a method for acquiring attitude parameters of a carrier before firing, and provides a method for acquiring the geographic location and attitude of a carrier by using an ultra-wideband sensor base station and a sensor tag, including the following steps: Coordinate system; Arrange sensor base stations around the launch position, and accurately locate the sensor base station in the geodetic coordinate system; Establish a carrier coordinate system; When the carrier enters the launch position, use the sensor base station to locate the sensor tag array: Use sensor tags The information calculates the transformation matrix between the geodetic coordinate system and the carrier coordinate system, and realizes the aiming calculation; the present invention introduces the geodetic coordinate system into the traditional UWB positioning, and combines the geodetic coordinate system with the position of the base station, so that the geographic location information of the carrier can be quickly obtained. It can replace the traditional aiming method to realize the process of obtaining the attitude parameters of the vehicle.
priorityDate 2022-02-11-04:00^^<http://www.w3.org/2001/XMLSchema#date>
type http://data.epo.org/linked-data/def/patent/Publication

Incoming Links

Predicate Subject
isDiscussedBy http://rdf.ncbi.nlm.nih.gov/pubchem/substance/SID422707724
http://rdf.ncbi.nlm.nih.gov/pubchem/compound/CID25078152
http://rdf.ncbi.nlm.nih.gov/pubchem/protein/ACCP27058

Total number of triples: 27.