| Predicate |
Object |
| assignee |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_7e1e5f6d940785204765c1d52d31a3fb |
| classificationCPCAdditional |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/G01S2205-008
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/G01S19-11
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/G01S19-258 |
| classificationCPCInventive |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/G01S5-0036
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/G01S19-42
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/G01S19-01
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/G01S19-09
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/G01S5-0018
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/G01S19-235
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/G01S19-27
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/G01S5-14 |
| classificationIPCAdditional |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/G01S19-11 |
| classificationIPCInventive |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/G01S19-27
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/G01S19-42
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/G01S5-00
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/G01S19-26
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/G01S19-25
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/G01S19-09
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/G01S19-24
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/G01S19-23
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/G01S1-00 |
| filingDate |
2005-03-10^^<http://www.w3.org/2001/XMLSchema#date> |
| grantDate |
2007-07-17^^<http://www.w3.org/2001/XMLSchema#date> |
| inventor |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_8522011774f572ec1fcb40e021114ca9
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_c4c0769403ca1ebc8d018e02e2e597f6 |
| publicationDate |
2007-07-17^^<http://www.w3.org/2001/XMLSchema#date> |
| publicationNumber |
US-7245253-B2 |
| titleOfInvention |
Method and apparatus for processing of satellite signals without time of day information |
| abstract |
Method and apparatus for locating position of a satellite signal receiver is described. In one example, pseudoranges are obtained that estimate the range of a satellite signal receiver to a plurality of satellites. An absolute time and a position are computed using the pseudoranges at a first time. The absolute time is then used to compute another position at a subsequent time. In another example, a plurality of states associated with a satellite signal receiver are estimated, where the plurality of states includes a time tag error state. A dynamic model is then formed relating the plurality of states, the dynamic model operative to compute position of the satellite signal receiver. |
| isCitedBy |
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-11428822-B2
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-8692712-B2
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-11675090-B1
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-10520606-B2 |
| priorityDate |
2000-11-17^^<http://www.w3.org/2001/XMLSchema#date> |
| type |
http://data.epo.org/linked-data/def/patent/Publication |