http://rdf.ncbi.nlm.nih.gov/pubchem/patent/WO-8701210-A1

Outgoing Links

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assignee http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_2c07e1223ebc79bc0680cb1f5b40b3cd
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classificationIPCInventive http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/G01S1-14
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/G01S13-78
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/G01S13-76
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/G01S13-86
filingDate 1986-08-12-04:00^^<http://www.w3.org/2001/XMLSchema#date>
inventor http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_d79b0b57821c56bf1cfe089e7f623aa3
publicationDate 1987-02-26-04:00^^<http://www.w3.org/2001/XMLSchema#date>
publicationNumber WO-8701210-A1
titleOfInvention Instrument landing system
abstract In a single-frequency precision guidance landing system, the use of a DME interrogator (50) in the aircraft and a DME receiver (60) at the ground installation, each tuned to the same DME channel frequency, to uniquely interrogate a selected ground station (29, 32, 21, 22, 33, 34) and hence identify it by virtue of its replies being synchronous in the aircraft (3, 8) with the interrogations, the interrogations and the replies also being used to obtain range to the ground installation. This technique uses airborne already-installed DME interrogators (50) for selective interrogation of a desired landing installation (60, 29, 32), thereby to eliminate any need to add additional special purpose equipment to the aircraft to accomplish the desired uniqueness of interrogation and ground installation identification achieved by this invention.
isCitedBy http://rdf.ncbi.nlm.nih.gov/pubchem/patent/CN-106019327-A
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-5113310-A
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/CN-105954767-A
priorityDate 1985-08-14-04:00^^<http://www.w3.org/2001/XMLSchema#date>
type http://data.epo.org/linked-data/def/patent/Publication

Incoming Links

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Total number of triples: 22.