FR2353893A1 - METHOD AND APPARATUS FOR GUIDING AERODYNE ON LANDING - Google Patents

METHOD AND APPARATUS FOR GUIDING AERODYNE ON LANDING

Info

Publication number
FR2353893A1
FR2353893A1 FR7612735A FR7612735A FR2353893A1 FR 2353893 A1 FR2353893 A1 FR 2353893A1 FR 7612735 A FR7612735 A FR 7612735A FR 7612735 A FR7612735 A FR 7612735A FR 2353893 A1 FR2353893 A1 FR 2353893A1
Authority
FR
France
Prior art keywords
aerodyne
landing
guiding
guiding aerodyne
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.)
Granted
Application number
FR7612735A
Other languages
French (fr)
Other versions
FR2353893B1 (en
Inventor
Jean-Marie Vauchy
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.)
Societe de Fabrication dInstruments de Mesure SFIM SA
Original Assignee
Societe de Fabrication dInstruments de Mesure SFIM SA
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 Societe de Fabrication dInstruments de Mesure SFIM SA filed Critical Societe de Fabrication dInstruments de Mesure SFIM SA
Priority to FR7612735A priority Critical patent/FR2353893A1/en
Priority to GB17137/77A priority patent/GB1572474A/en
Priority to DE2718698A priority patent/DE2718698C2/en
Publication of FR2353893A1 publication Critical patent/FR2353893A1/en
Application granted granted Critical
Publication of FR2353893B1 publication Critical patent/FR2353893B1/fr
Granted 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
    • G01S3/00—Direction-finders for determining the direction from which infrasonic, sonic, ultrasonic, or electromagnetic waves, or particle emission, not having a directional significance, are being received
    • G01S3/78—Direction-finders for determining the direction from which infrasonic, sonic, ultrasonic, or electromagnetic waves, or particle emission, not having a directional significance, are being received using electromagnetic waves other than radio waves
    • G01S3/782—Systems for determining direction or deviation from predetermined direction
    • G01S3/785—Systems for determining direction or deviation from predetermined direction using adjustment of orientation of directivity characteristics of a detector or detector system to give a desired condition of signal derived from that detector or detector system
    • G01S3/786—Systems for determining direction or deviation from predetermined direction using adjustment of orientation of directivity characteristics of a detector or detector system to give a desired condition of signal derived from that detector or detector system the desired condition being maintained automatically
    • G01S3/7864—T.V. type tracking systems
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
    • G05D1/04—Control of altitude or depth
    • G05D1/06—Rate of change of altitude or depth
    • G05D1/0607—Rate of change of altitude or depth specially adapted for aircraft
    • G05D1/0653—Rate of change of altitude or depth specially adapted for aircraft during a phase of take-off or landing
    • G05D1/0676—Rate of change of altitude or depth specially adapted for aircraft during a phase of take-off or landing specially adapted for landing
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
    • G05D1/08—Control of attitude, i.e. control of roll, pitch, or yaw
    • G05D1/0808—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft
    • G05D1/0858—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft specially adapted for vertical take-off of aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • General Physics & Mathematics (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Automation & Control Theory (AREA)
  • Electromagnetism (AREA)
  • Length Measuring Devices By Optical Means (AREA)
FR7612735A 1976-04-29 1976-04-29 METHOD AND APPARATUS FOR GUIDING AERODYNE ON LANDING Granted FR2353893A1 (en)

Priority Applications (3)

Application Number Priority Date Filing Date Title
FR7612735A FR2353893A1 (en) 1976-04-29 1976-04-29 METHOD AND APPARATUS FOR GUIDING AERODYNE ON LANDING
GB17137/77A GB1572474A (en) 1976-04-29 1977-04-25 Method of guiding aerodynes when landing
DE2718698A DE2718698C2 (en) 1976-04-29 1977-04-27 Procedures for commanding aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR7612735A FR2353893A1 (en) 1976-04-29 1976-04-29 METHOD AND APPARATUS FOR GUIDING AERODYNE ON LANDING

Publications (2)

Publication Number Publication Date
FR2353893A1 true FR2353893A1 (en) 1977-12-30
FR2353893B1 FR2353893B1 (en) 1982-08-27

Family

ID=9172455

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7612735A Granted FR2353893A1 (en) 1976-04-29 1976-04-29 METHOD AND APPARATUS FOR GUIDING AERODYNE ON LANDING

Country Status (3)

Country Link
DE (1) DE2718698C2 (en)
FR (1) FR2353893A1 (en)
GB (1) GB1572474A (en)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3644478A1 (en) * 1986-12-24 1988-07-07 Licentia Gmbh SYSTEM FOR LANDING AID FOR AIRCRAFT WITH OWN ON-BOARD RADAR
DE102007019806A1 (en) * 2007-04-26 2009-05-14 Esg Elektroniksystem- Und Logistik-Gmbh Helicopter's horizontal movement condition determining device, has ground detection device i.e. infrared camera, which is provided at helicopter, where device detects predetermined ground area
US9891632B1 (en) * 2016-08-15 2018-02-13 The Boeing Company Point-and-shoot automatic landing system and method

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1404404A (en) * 1961-09-22 1965-07-02 Bristol Aircraft Ltd Advanced missile guidance
FR1605307A (en) * 1964-06-23 1974-08-02

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
NO130339B (en) * 1970-11-13 1974-08-12 Saab Scania Ab
DE2238615C2 (en) * 1972-08-05 1974-03-07 Messerschmitt-Boelkow-Blohm Gmbh, 8000 Muenchen On-board autonomous bad weather landing procedure

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1404404A (en) * 1961-09-22 1965-07-02 Bristol Aircraft Ltd Advanced missile guidance
FR1605307A (en) * 1964-06-23 1974-08-02

Also Published As

Publication number Publication date
DE2718698C2 (en) 1981-11-12
DE2718698A1 (en) 1977-11-10
GB1572474A (en) 1980-07-30
FR2353893B1 (en) 1982-08-27

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Legal Events

Date Code Title Description
ST Notification of lapse