GB1434305A - Aircraft control system using inertial signals - Google Patents

Aircraft control system using inertial signals

Info

Publication number
GB1434305A
GB1434305A GB2410673A GB2410673A GB1434305A GB 1434305 A GB1434305 A GB 1434305A GB 2410673 A GB2410673 A GB 2410673A GB 2410673 A GB2410673 A GB 2410673A GB 1434305 A GB1434305 A GB 1434305A
Authority
GB
United Kingdom
Prior art keywords
aircraft
signal
produce
control
signals
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
GB2410673A
Other languages
English (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.)
Bendix Corp
Original Assignee
Bendix 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 Bendix Corp filed Critical Bendix Corp
Publication of GB1434305A publication Critical patent/GB1434305A/en
Expired 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)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Position Fixing By Use Of Radio Waves (AREA)
  • Traffic Control Systems (AREA)
GB2410673A 1972-05-25 1973-05-21 Aircraft control system using inertial signals Expired GB1434305A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US00256897A US3824381A (en) 1972-05-25 1972-05-25 Aircraft control system using inertial signals

Publications (1)

Publication Number Publication Date
GB1434305A true GB1434305A (en) 1976-05-05

Family

ID=22974058

Family Applications (1)

Application Number Title Priority Date Filing Date
GB2410673A Expired GB1434305A (en) 1972-05-25 1973-05-21 Aircraft control system using inertial signals

Country Status (6)

Country Link
US (1) US3824381A (enExample)
JP (1) JPS56280B2 (enExample)
CA (1) CA1000837A (enExample)
DE (1) DE2326831A1 (enExample)
FR (1) FR2185798B1 (enExample)
GB (1) GB1434305A (enExample)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3897031A (en) * 1974-03-15 1975-07-29 Bendix Corp Apparatus for providing selected navigational system engage logic
US3989209A (en) * 1974-06-26 1976-11-02 The Bendix Corporation Apparatus for guiding an aircraft along a multi-segment path when landing the craft
JPS5228041A (en) * 1975-08-29 1977-03-02 Nissan Motor Co Ltd Wear-resistant sliding member
US5023796A (en) * 1989-10-03 1991-06-11 Honeywell, Inc. Flight control apparatus with predictive heading/track hold command
US6450456B1 (en) 1999-12-20 2002-09-17 Safe Flight Instrument Corporation Airborne safe landing power control system and method
FR2847553B1 (fr) 2002-11-27 2004-12-31 Eurocopter France Dispositif d'aide a l'interception par un aeronef d'un segment d'une trajectoire situee dans un plan horizontal et systeme d'aide a l'interception et au suivi d'un tel segment

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3058699A (en) * 1961-04-06 1962-10-16 Sperry Rand Corp Automatic approach system for aircraft
US3223362A (en) * 1963-08-21 1965-12-14 Bendix Corp Flight control apparatus
US3327973A (en) * 1965-06-14 1967-06-27 Lear Siegler Inc Automatic landing pitch axis control system for aircraft
US3291421A (en) * 1965-09-20 1966-12-13 Lear Siegler Inc Pitch controller for automatic landing
US3361392A (en) * 1965-10-05 1968-01-02 Bendix Corp Aircraft control system for lateral runway alignment
US3417945A (en) * 1965-11-30 1968-12-24 Bendix Corp Aircraft control system for lateral runway alignment
US3467344A (en) * 1967-08-25 1969-09-16 Lear Siegler Inc Automatic landing control system having improved wind shear capability
US3604908A (en) * 1969-05-19 1971-09-14 Sperry Rand Corp Landing control system for aircraft
US3743221A (en) * 1970-04-09 1973-07-03 Lear Siegler Inc Aircraft flight control apparatus
US3652835A (en) * 1970-05-14 1972-03-28 Sperry Rand Corp Aircraft glide slope coupler system
US3697022A (en) * 1970-07-06 1972-10-10 Sfim Method and apparatus for aircraft guidance

Also Published As

Publication number Publication date
CA1000837A (en) 1976-11-30
FR2185798B1 (enExample) 1977-07-29
JPS4942100A (enExample) 1974-04-20
DE2326831A1 (de) 1973-12-06
US3824381A (en) 1974-07-16
FR2185798A1 (enExample) 1974-01-04
JPS56280B2 (enExample) 1981-01-07

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Legal Events

Date Code Title Description
PS Patent sealed [section 19, patents act 1949]
PCNP Patent ceased through non-payment of renewal fee