DE69502829T2 - System zur positionsbestimmung und identifizierung von luftfahrzeugen - Google Patents

System zur positionsbestimmung und identifizierung von luftfahrzeugen

Info

Publication number
DE69502829T2
DE69502829T2 DE69502829T DE69502829T DE69502829T2 DE 69502829 T2 DE69502829 T2 DE 69502829T2 DE 69502829 T DE69502829 T DE 69502829T DE 69502829 T DE69502829 T DE 69502829T DE 69502829 T2 DE69502829 T2 DE 69502829T2
Authority
DE
Germany
Prior art keywords
aircraft
identification
determining
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
DE69502829T
Other languages
English (en)
Other versions
DE69502829D1 (de
Inventor
Robert Coles
Ronald Langietti
Dennis Vaccaro
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Northrop Grumman Corp
Original Assignee
Northrop Grumman Corp
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Northrop Grumman Corp filed Critical Northrop Grumman Corp
Publication of DE69502829D1 publication Critical patent/DE69502829D1/de
Application granted granted Critical
Publication of DE69502829T2 publication Critical patent/DE69502829T2/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • G—PHYSICS
    • G08—SIGNALLING
    • G08G—TRAFFIC CONTROL SYSTEMS
    • G08G5/00—Traffic control systems for aircraft, e.g. air-traffic control [ATC]
    • G08G5/0047—Navigation or guidance aids for a single aircraft
    • G08G5/0052—Navigation or guidance aids for a single aircraft for cruising
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
    • G01S19/00—Satellite radio beacon positioning systems; Determining position, velocity or attitude using signals transmitted by such systems
    • G01S19/01—Satellite radio beacon positioning systems transmitting time-stamped messages, e.g. GPS [Global Positioning System], GLONASS [Global Orbiting Navigation Satellite System] or GALILEO
    • G01S19/13—Receivers
    • G01S19/14—Receivers specially adapted for specific applications
    • G01S19/15—Aircraft landing systems
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
    • G01S19/00—Satellite radio beacon positioning systems; Determining position, velocity or attitude using signals transmitted by such systems
    • G01S19/38—Determining a navigation solution using signals transmitted by a satellite radio beacon positioning system
    • G01S19/39—Determining a navigation solution using signals transmitted by a satellite radio beacon positioning system the satellite radio beacon positioning system transmitting time-stamped messages, e.g. GPS [Global Positioning System], GLONASS [Global Orbiting Navigation Satellite System] or GALILEO
    • G01S19/42—Determining position
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
    • G01S5/00—Position-fixing by co-ordinating two or more direction or position line determinations; Position-fixing by co-ordinating two or more distance determinations
    • G01S5/0009—Transmission of position information to remote stations
    • G—PHYSICS
    • G08—SIGNALLING
    • G08G—TRAFFIC CONTROL SYSTEMS
    • G08G5/00—Traffic control systems for aircraft, e.g. air-traffic control [ATC]
    • G08G5/0004—Transmission of traffic-related information to or from an aircraft
    • G08G5/0008—Transmission of traffic-related information to or from an aircraft with other aircraft
    • G—PHYSICS
    • G08—SIGNALLING
    • G08G—TRAFFIC CONTROL SYSTEMS
    • G08G5/00—Traffic control systems for aircraft, e.g. air-traffic control [ATC]
    • G08G5/0004—Transmission of traffic-related information to or from an aircraft
    • G08G5/0013—Transmission of traffic-related information to or from an aircraft with a ground station
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
    • G01S19/00—Satellite radio beacon positioning systems; Determining position, velocity or attitude using signals transmitted by such systems
    • G01S19/38—Determining a navigation solution using signals transmitted by a satellite radio beacon positioning system
    • G01S19/39—Determining a navigation solution using signals transmitted by a satellite radio beacon positioning system the satellite radio beacon positioning system transmitting time-stamped messages, e.g. GPS [Global Positioning System], GLONASS [Global Orbiting Navigation Satellite System] or GALILEO
    • G01S19/42—Determining position
    • G01S19/48—Determining position by combining or switching between position solutions derived from the satellite radio beacon positioning system and position solutions derived from a further system
    • G01S19/49—Determining position by combining or switching between position solutions derived from the satellite radio beacon positioning system and position solutions derived from a further system whereby the further system is an inertial position system, e.g. loosely-coupled
DE69502829T 1994-04-19 1995-04-13 System zur positionsbestimmung und identifizierung von luftfahrzeugen Expired - Lifetime DE69502829T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US22970194A 1994-04-19 1994-04-19
PCT/US1995/004648 WO1995028650A1 (en) 1994-04-19 1995-04-13 Aircraft location and identification system

Publications (2)

Publication Number Publication Date
DE69502829D1 DE69502829D1 (de) 1998-07-09
DE69502829T2 true DE69502829T2 (de) 1999-02-25

Family

ID=22862360

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69502829T Expired - Lifetime DE69502829T2 (de) 1994-04-19 1995-04-13 System zur positionsbestimmung und identifizierung von luftfahrzeugen

Country Status (5)

Country Link
US (1) US5596332A (de)
EP (1) EP0760955B1 (de)
JP (1) JP3751021B2 (de)
DE (1) DE69502829T2 (de)
WO (1) WO1995028650A1 (de)

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Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
AT521474B1 (de) * 2018-10-24 2020-02-15 Frequentis Ag Verfahren zur Erkennung von Luftfahrzeugen
AT521474A4 (de) * 2018-10-24 2020-02-15 Frequentis Ag Verfahren zur Erkennung von Luftfahrzeugen

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JPH10501059A (ja) 1998-01-27
EP0760955A1 (de) 1997-03-12
EP0760955B1 (de) 1998-06-03
WO1995028650A1 (en) 1995-10-26
DE69502829D1 (de) 1998-07-09
EP0760955A4 (de) 1997-06-25
JP3751021B2 (ja) 2006-03-01
US5596332A (en) 1997-01-21

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