FR2344001A2 - Aircraft control equipment for landing approach - has controller with indicators for altitude-time settings and for starting deceleration procedure - Google Patents

Aircraft control equipment for landing approach - has controller with indicators for altitude-time settings and for starting deceleration procedure

Info

Publication number
FR2344001A2
FR2344001A2 FR7606592A FR7606592A FR2344001A2 FR 2344001 A2 FR2344001 A2 FR 2344001A2 FR 7606592 A FR7606592 A FR 7606592A FR 7606592 A FR7606592 A FR 7606592A FR 2344001 A2 FR2344001 A2 FR 2344001A2
Authority
FR
France
Prior art keywords
altitude
aircraft
pilot
indicators
controller
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
FR7606592A
Other languages
French (fr)
Other versions
FR2344001B2 (en
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 Francaise dEquipements pour la Navigation Aerienne SFENA SA
Original Assignee
Societe Francaise dEquipements pour la Navigation Aerienne SFENA 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 Francaise dEquipements pour la Navigation Aerienne SFENA SA filed Critical Societe Francaise dEquipements pour la Navigation Aerienne SFENA SA
Priority to FR7606592A priority Critical patent/FR2344001A2/en
Publication of FR2344001A2 publication Critical patent/FR2344001A2/en
Application granted granted Critical
Publication of FR2344001B2 publication Critical patent/FR2344001B2/fr
Granted legal-status Critical Current

Links

Classifications

    • 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
    • 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
    • G01S1/00—Beacons or beacon systems transmitting signals having a characteristic or characteristics capable of being detected by non-directional receivers and defining directions, positions, or position lines fixed relatively to the beacon transmitters; Receivers co-operating therewith
    • G01S1/02—Beacons or beacon systems transmitting signals having a characteristic or characteristics capable of being detected by non-directional receivers and defining directions, positions, or position lines fixed relatively to the beacon transmitters; Receivers co-operating therewith using radio waves

Landscapes

  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Computer Networks & Wireless Communication (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Automation & Control Theory (AREA)
  • Traffic Control Systems (AREA)

Abstract

An equipment is used to control the landing approach of an aircraft along its guide path. It controls the deceleration during the deceleration phase of the aircraft. It also indicates to the pilot whether correction is required of the deviation between the total slope and the reference slope. The equipment comprises a display (3) with two indicators (2, 4). When the pilot proceeds with the procedure of glide path capture, he presses the triangle indicator to start the decelerated approach equipment. When the aircraft is at a given first altitude, and first instant in time, the arrow indicator lights-up and informs the pilot to initiate the first deceleration phase and to lower the undercarriage, reset the wing flaps and adjust the engine throttle. When the aircraft is at a given second altitude and instant, the arrow indicator again nforms the pilot to reset the wing flaps.
FR7606592A 1976-03-08 1976-03-08 Aircraft control equipment for landing approach - has controller with indicators for altitude-time settings and for starting deceleration procedure Granted FR2344001A2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR7606592A FR2344001A2 (en) 1976-03-08 1976-03-08 Aircraft control equipment for landing approach - has controller with indicators for altitude-time settings and for starting deceleration procedure

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR7606592A FR2344001A2 (en) 1976-03-08 1976-03-08 Aircraft control equipment for landing approach - has controller with indicators for altitude-time settings and for starting deceleration procedure

Publications (2)

Publication Number Publication Date
FR2344001A2 true FR2344001A2 (en) 1977-10-07
FR2344001B2 FR2344001B2 (en) 1980-09-26

Family

ID=9170108

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7606592A Granted FR2344001A2 (en) 1976-03-08 1976-03-08 Aircraft control equipment for landing approach - has controller with indicators for altitude-time settings and for starting deceleration procedure

Country Status (1)

Country Link
FR (1) FR2344001A2 (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2958050A1 (en) * 2010-03-24 2011-09-30 Dassault Aviat METHOD AND SYSTEM FOR MANAGING THE ENERGY VARIATION OF AN AIRCRAFT
US8706324B2 (en) 2010-03-24 2014-04-22 Dassault Aviation Device for displaying the energy variation of an aircraft, corresponding method and system for displaying the energy variation
US11358733B2 (en) 2020-01-21 2022-06-14 Rockwell Collins, Inc. Optimum idle descent start point display based on current conditions

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2958050A1 (en) * 2010-03-24 2011-09-30 Dassault Aviat METHOD AND SYSTEM FOR MANAGING THE ENERGY VARIATION OF AN AIRCRAFT
US8527173B2 (en) 2010-03-24 2013-09-03 Dassault Aviation Method and system for managing the energy variation of an aircraft
US8706324B2 (en) 2010-03-24 2014-04-22 Dassault Aviation Device for displaying the energy variation of an aircraft, corresponding method and system for displaying the energy variation
US11358733B2 (en) 2020-01-21 2022-06-14 Rockwell Collins, Inc. Optimum idle descent start point display based on current conditions

Also Published As

Publication number Publication date
FR2344001B2 (en) 1980-09-26

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