http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-5241319-A

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assignee http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_5547f741b25666fc4ae5195cf71a979b
classificationCPCInventive http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/H01Q3-02
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/H01Q1-3275
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/H01Q3-2605
classificationIPCInventive http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/G01S3-40
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/H01Q1-32
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/H01Q3-02
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/H01Q1-27
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/H01Q3-26
filingDate 1991-04-19^^<http://www.w3.org/2001/XMLSchema#date>
grantDate 1993-08-31^^<http://www.w3.org/2001/XMLSchema#date>
inventor http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_be4a1ca4fd8db4e94dc1c6ef5afd04e4
publicationDate 1993-08-31^^<http://www.w3.org/2001/XMLSchema#date>
publicationNumber US-5241319-A
titleOfInvention Antenna beam pointing method for satellite mobile communications system
abstract A method for tracking a satellite in a land mobile satellite communications system is disclosed. A rate gyro is provided for use in the event that an automatic satellite tracking is prevented. The satellite is automatically tracked using a receive signal level if the receive signal level equals or exceeds a threshold. An output of the rate gyro is constantly compensated while automatically tracking the satellite. When the receive signal level falls below the threshold and the automatic satellite tracking becomes unable, the satellite is tracked using the compensated output of the rate gyro.
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http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-6052084-A
priorityDate 1990-04-19^^<http://www.w3.org/2001/XMLSchema#date>
type http://data.epo.org/linked-data/def/patent/Publication

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