DE1234537B - Flugzeuglandeeinrichtung - Google Patents

Flugzeuglandeeinrichtung

Info

Publication number
DE1234537B
DE1234537B DEN20078A DEN0020078A DE1234537B DE 1234537 B DE1234537 B DE 1234537B DE N20078 A DEN20078 A DE N20078A DE N0020078 A DEN0020078 A DE N0020078A DE 1234537 B DE1234537 B DE 1234537B
Authority
DE
Germany
Prior art keywords
descent
rate
signal
output
summing
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.)
Pending
Application number
DEN20078A
Other languages
German (de)
English (en)
Inventor
Elliott Robbin Buxton
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.)
North American Aviation Corp
Original Assignee
North American Aviation 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 North American Aviation Corp filed Critical North American Aviation Corp
Publication of DE1234537B publication Critical patent/DE1234537B/de
Pending 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)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Automation & Control Theory (AREA)
  • Computer Networks & Wireless Communication (AREA)
  • Radar Systems Or Details Thereof (AREA)
  • Feedback Control In General (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
DEN20078A 1960-06-10 1961-05-23 Flugzeuglandeeinrichtung Pending DE1234537B (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US35306A US3059880A (en) 1960-06-10 1960-06-10 Terminal predication aircraft landing system

Publications (1)

Publication Number Publication Date
DE1234537B true DE1234537B (de) 1967-02-16

Family

ID=21881838

Family Applications (1)

Application Number Title Priority Date Filing Date
DEN20078A Pending DE1234537B (de) 1960-06-10 1961-05-23 Flugzeuglandeeinrichtung

Country Status (5)

Country Link
US (1) US3059880A (enExample)
DE (1) DE1234537B (enExample)
FR (1) FR1300183A (enExample)
GB (1) GB964595A (enExample)
SE (1) SE306671B (enExample)

Families Citing this family (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3126175A (en) * 1964-03-24 Lowell
US3230351A (en) * 1960-09-14 1966-01-18 Bendix Corp Self-adaptive control system
GB1007890A (en) * 1962-01-11 1965-10-22 Communications Patents Ltd Improvements in or relating to ground-based flight training apparatus
NL288436A (enExample) * 1962-02-02
US3169730A (en) * 1962-11-01 1965-02-16 Sperry Rand Corp Flight control system
GB1065695A (en) * 1963-01-18 1967-04-19 Smiths Industries Ltd Improvements in or relating to automatic flight control systems for aircraft
US3277355A (en) * 1963-12-23 1966-10-04 Gen Electric Terminal condition predictive control system
US3523664A (en) * 1968-03-28 1970-08-11 Bendix Corp Terminal flare controller
US3523663A (en) * 1968-03-28 1970-08-11 Bendix Corp Terminal flare controller
US3805033A (en) * 1972-11-20 1974-04-16 Collins Radio Co Autopilot go-around mode pitch command signal computations
US4413320A (en) * 1980-08-22 1983-11-01 The Bendix Corporation Control system
CN103991553B (zh) * 2013-02-19 2016-02-24 成都海存艾匹科技有限公司 飞机精准着陆辅助装置
DE102014014446A1 (de) * 2014-09-26 2016-03-31 Airbus Defence and Space GmbH Redundantes Bestimmen von Positionsdaten für ein automatisches Landesystem
CN114355824A (zh) * 2022-01-18 2022-04-15 中国人民解放军空军工程大学航空机务士官学校 一种智能化飞机着陆装置检测仪

Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2592173A (en) * 1946-10-25 1952-04-08 Bendix Aviat Corp Automatic control of mobile craft
US2800292A (en) * 1948-05-12 1957-07-23 Collins Radio Co Automatic landing system
US2808999A (en) * 1949-05-07 1957-10-08 Sperry Rand Corp Automatic flight control apparatus
DE1029238B (de) 1955-12-06 1958-04-30 Sperry Rand Corp Steuervorrichtung in Flugzeugen zur Verhinderung von Auftriebsstoessen
US2834564A (en) * 1947-09-19 1958-05-13 Bendix Aviat Corp Orientation control
US2861757A (en) * 1953-06-01 1958-11-25 Honeywell Regulator Co Interlocking apparatus for radio control of aircraft
DE1067310B (enExample) 1959-10-15
US2936134A (en) * 1956-03-15 1960-05-10 Sperry Rand Corp Longitudinal axis control system for aircraft
US2940032A (en) * 1952-08-29 1960-06-07 Wiesing Ab Instrument landing system
DE1099361B (de) 1952-08-29 1961-02-09 Wiesing Ab Vorrichtung fuer die Ableitung von Steuerkommandos zum Heranfuehren eines Luftfahrzeuges an einen Leitstrahl

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2841345A (en) * 1952-01-15 1958-07-01 Sperry Rand Corp Glide path system with flare out
US2830291A (en) * 1954-09-23 1958-04-08 Sperry Rand Corp Flare-out control

Patent Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1067310B (enExample) 1959-10-15
US2592173A (en) * 1946-10-25 1952-04-08 Bendix Aviat Corp Automatic control of mobile craft
US2834564A (en) * 1947-09-19 1958-05-13 Bendix Aviat Corp Orientation control
US2800292A (en) * 1948-05-12 1957-07-23 Collins Radio Co Automatic landing system
US2808999A (en) * 1949-05-07 1957-10-08 Sperry Rand Corp Automatic flight control apparatus
US2940032A (en) * 1952-08-29 1960-06-07 Wiesing Ab Instrument landing system
DE1099361B (de) 1952-08-29 1961-02-09 Wiesing Ab Vorrichtung fuer die Ableitung von Steuerkommandos zum Heranfuehren eines Luftfahrzeuges an einen Leitstrahl
US2861757A (en) * 1953-06-01 1958-11-25 Honeywell Regulator Co Interlocking apparatus for radio control of aircraft
DE1029238B (de) 1955-12-06 1958-04-30 Sperry Rand Corp Steuervorrichtung in Flugzeugen zur Verhinderung von Auftriebsstoessen
US2936134A (en) * 1956-03-15 1960-05-10 Sperry Rand Corp Longitudinal axis control system for aircraft

Also Published As

Publication number Publication date
SE306671B (enExample) 1968-12-02
GB964595A (en) 1964-07-22
FR1300183A (fr) 1962-08-03
US3059880A (en) 1962-10-23

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