DE69213041T2 - Integriertes Flug- und Anflug-Leitsystem für Luftfahrzeuge - Google Patents

Integriertes Flug- und Anflug-Leitsystem für Luftfahrzeuge

Info

Publication number
DE69213041T2
DE69213041T2 DE69213041T DE69213041T DE69213041T2 DE 69213041 T2 DE69213041 T2 DE 69213041T2 DE 69213041 T DE69213041 T DE 69213041T DE 69213041 T DE69213041 T DE 69213041T DE 69213041 T2 DE69213041 T2 DE 69213041T2
Authority
DE
Germany
Prior art keywords
aircraft
control system
approach control
integrated flight
flight
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 - Fee Related
Application number
DE69213041T
Other languages
English (en)
Other versions
DE69213041D1 (de
Inventor
Kenneth W Mcelereath
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.)
Boeing North American Inc
Original Assignee
Rockwell International 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 Rockwell International Corp filed Critical Rockwell International Corp
Publication of DE69213041D1 publication Critical patent/DE69213041D1/de
Application granted granted Critical
Publication of DE69213041T2 publication Critical patent/DE69213041T2/de
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • 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
    • G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C21/00—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00
    • G01C21/10—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 by using measurements of speed or acceleration
    • G01C21/12—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 by using measurements of speed or acceleration executed aboard the object being navigated; Dead reckoning
    • G01C21/16—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 by using measurements of speed or acceleration executed aboard the object being navigated; Dead reckoning by integrating acceleration or speed, i.e. inertial navigation
    • G01C21/165—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 by using measurements of speed or acceleration executed aboard the object being navigated; Dead reckoning by integrating acceleration or speed, i.e. inertial navigation combined with non-inertial navigation instruments
    • G01C21/1652—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 by using measurements of speed or acceleration executed aboard the object being navigated; Dead reckoning by integrating acceleration or speed, i.e. inertial navigation combined with non-inertial navigation instruments with ranging devices, e.g. LIDAR or RADAR
    • 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
DE69213041T 1991-02-08 1992-02-07 Integriertes Flug- und Anflug-Leitsystem für Luftfahrzeuge Expired - Fee Related DE69213041T2 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US07/652,762 US5216611A (en) 1991-02-08 1991-02-08 Integrated enroute and approach guidance system for aircraft

Publications (2)

Publication Number Publication Date
DE69213041D1 DE69213041D1 (de) 1996-10-02
DE69213041T2 true DE69213041T2 (de) 1997-03-27

Family

ID=24618046

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69213041T Expired - Fee Related DE69213041T2 (de) 1991-02-08 1992-02-07 Integriertes Flug- und Anflug-Leitsystem für Luftfahrzeuge

Country Status (4)

Country Link
US (1) US5216611A (de)
EP (1) EP0498655B1 (de)
JP (1) JP3162156B2 (de)
DE (1) DE69213041T2 (de)

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Also Published As

Publication number Publication date
EP0498655A3 (en) 1992-10-21
DE69213041D1 (de) 1996-10-02
JPH06224697A (ja) 1994-08-12
EP0498655B1 (de) 1996-08-28
EP0498655A2 (de) 1992-08-12
US5216611A (en) 1993-06-01
JP3162156B2 (ja) 2001-04-25

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