DE1774213C3 - Flugnavigationshilfsanordnung - Google Patents

Flugnavigationshilfsanordnung

Info

Publication number
DE1774213C3
DE1774213C3 DE1774213A DE1774213A DE1774213C3 DE 1774213 C3 DE1774213 C3 DE 1774213C3 DE 1774213 A DE1774213 A DE 1774213A DE 1774213 A DE1774213 A DE 1774213A DE 1774213 C3 DE1774213 C3 DE 1774213C3
Authority
DE
Germany
Prior art keywords
aircraft
value
altitude
flight path
inclination
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
Application number
DE1774213A
Other languages
German (de)
English (en)
Other versions
DE1774213B2 (de
DE1774213A1 (de
Inventor
Georges Colombet
Rene Lami
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.)
Thales SA
Original Assignee
CSF Compagnie Generale de Telegraphie sans Fil 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 CSF Compagnie Generale de Telegraphie sans Fil SA filed Critical CSF Compagnie Generale de Telegraphie sans Fil SA
Publication of DE1774213A1 publication Critical patent/DE1774213A1/de
Publication of DE1774213B2 publication Critical patent/DE1774213B2/de
Application granted granted Critical
Publication of DE1774213C3 publication Critical patent/DE1774213C3/de
Expired legal-status Critical Current

Links

Classifications

    • GPHYSICS
    • G06COMPUTING OR CALCULATING; COUNTING
    • G06GANALOGUE COMPUTERS
    • G06G7/00Devices in which the computing operation is performed by varying electric or magnetic quantities
    • G06G7/48Analogue computers for specific processes, systems or devices, e.g. simulators
    • G06G7/78Analogue computers for specific processes, systems or devices, e.g. simulators for direction-finding, locating, distance or velocity measuring, or navigation systems
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01SRADIO 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
    • G01S1/00Beacons 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
    • G01S1/02Beacons 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
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01SRADIO 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
    • G01S13/00Systems using the reflection or reradiation of radio waves, e.g. radar systems; Analogous systems using reflection or reradiation of waves whose nature or wavelength is irrelevant or unspecified
    • G01S13/88Radar or analogous systems specially adapted for specific applications
    • G01S13/91Radar or analogous systems specially adapted for specific applications for traffic control
    • G01S13/913Radar or analogous systems specially adapted for specific applications for traffic control for landing purposes
    • GPHYSICS
    • G05CONTROLLING; REGULATING
    • G05DSYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
    • G05D1/04Control of altitude or depth
    • G05D1/06Rate of change of altitude or depth
    • G05D1/0607Rate of change of altitude or depth specially adapted for aircraft
    • G05D1/0653Rate of change of altitude or depth specially adapted for aircraft during a phase of take-off or landing
    • GPHYSICS
    • G05CONTROLLING; REGULATING
    • G05DSYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
    • G05D1/04Control of altitude or depth
    • G05D1/06Rate of change of altitude or depth
    • G05D1/0607Rate of change of altitude or depth specially adapted for aircraft
    • G05D1/0653Rate of change of altitude or depth specially adapted for aircraft during a phase of take-off or landing
    • G05D1/0676Rate of change of altitude or depth specially adapted for aircraft during a phase of take-off or landing specially adapted for landing

Landscapes

  • Engineering & Computer Science (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Theoretical Computer Science (AREA)
  • Computer Hardware Design (AREA)
  • Automation & Control Theory (AREA)
  • Computer Networks & Wireless Communication (AREA)
  • Mathematical Physics (AREA)
  • Electromagnetism (AREA)
  • Traffic Control Systems (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Radar Systems Or Details Thereof (AREA)
  • Navigation (AREA)
DE1774213A 1967-05-03 1968-05-03 Flugnavigationshilfsanordnung Expired DE1774213C3 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR105164A FR92519E (fr) 1967-05-03 1967-05-03 Calculateur de pente vraie

Publications (3)

Publication Number Publication Date
DE1774213A1 DE1774213A1 (de) 1971-07-29
DE1774213B2 DE1774213B2 (de) 1973-09-20
DE1774213C3 true DE1774213C3 (de) 1974-06-20

Family

ID=8630173

Family Applications (1)

Application Number Title Priority Date Filing Date
DE1774213A Expired DE1774213C3 (de) 1967-05-03 1968-05-03 Flugnavigationshilfsanordnung

Country Status (4)

Country Link
US (1) US3588477A (enExample)
DE (1) DE1774213C3 (enExample)
FR (1) FR92519E (enExample)
GB (1) GB1232601A (enExample)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3624366A (en) * 1969-01-29 1971-11-30 Kollsman Instr Corp Vertical flight path error altimeter
US3735341A (en) * 1970-08-27 1973-05-22 Lear Siegler Inc Altitude alerting apparatus
US3911436A (en) * 1972-10-10 1975-10-07 Bodenseewerk Geraetetech Device for aircraft trajectory guidance
US3862717A (en) * 1973-08-09 1975-01-28 King Radio Corp Method and apparatus for automatically computing vertical track angle
US4387360A (en) * 1979-09-14 1983-06-07 Jourdan Ray M Glidepath system for use with aircraft altimeters

Also Published As

Publication number Publication date
DE1774213B2 (de) 1973-09-20
FR92519E (fr) 1968-11-22
GB1232601A (enExample) 1971-05-19
DE1774213A1 (de) 1971-07-29
US3588477A (en) 1971-06-28

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Legal Events

Date Code Title Description
C3 Grant after two publication steps (3rd publication)
E77 Valid patent as to the heymanns-index 1977
EHJ Ceased/non-payment of the annual fee