GB1520391A - Method and apparatus for automatic heading control - Google Patents

Method and apparatus for automatic heading control

Info

Publication number
GB1520391A
GB1520391A GB1326/77A GB132677A GB1520391A GB 1520391 A GB1520391 A GB 1520391A GB 1326/77 A GB1326/77 A GB 1326/77A GB 132677 A GB132677 A GB 132677A GB 1520391 A GB1520391 A GB 1520391A
Authority
GB
United Kingdom
Prior art keywords
control
aircraft
manual
automatic
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
GB1326/77A
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.)
Raytheon Technologies Corp
Original Assignee
United Technologies 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
Priority claimed from US05/649,331 external-priority patent/US4067517A/en
Priority claimed from US05/666,590 external-priority patent/US4003532A/en
Application filed by United Technologies Corp filed Critical United Technologies Corp
Publication of GB1520391A publication Critical patent/GB1520391A/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
    • G05D1/0055—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots with safety arrangements
    • G05D1/0061—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots with safety arrangements for transition from automatic pilot to manual pilot and vice versa

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Automation & Control Theory (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Toys (AREA)
GB1326/77A 1976-02-03 1977-01-13 Method and apparatus for automatic heading control Expired GB1520391A (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US05/649,331 US4067517A (en) 1976-02-03 1976-02-03 Automatic heading synchronization control system
US05/666,590 US4003532A (en) 1976-03-15 1976-03-15 Heading hold logic

Publications (1)

Publication Number Publication Date
GB1520391A true GB1520391A (en) 1978-08-09

Family

ID=27095583

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1326/77A Expired GB1520391A (en) 1976-02-03 1977-01-13 Method and apparatus for automatic heading control

Country Status (6)

Country Link
JP (1) JPS5288999A (ja)
DE (1) DE2701564A1 (ja)
FR (1) FR2340589A1 (ja)
GB (1) GB1520391A (ja)
IL (1) IL51185A (ja)
IT (1) IT1079172B (ja)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2262725A (en) * 1991-12-27 1993-06-30 Keith Trevor Lawes Externally referenced rotary wing cyclic pitch control.
US11679865B2 (en) 2021-06-21 2023-06-20 Honeywell International Inc. Aircraft yoke interference detection system and method

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4312039A (en) * 1980-01-24 1982-01-19 Sperry Corporation Transient free synchronization system
US4382283A (en) * 1980-08-08 1983-05-03 United Technologies Corporation Helicopter attitude and airspeed acquisition and retention system
FR2647922B1 (fr) * 1989-05-31 1993-12-31 Sextant Avionique Dispositif de commande electromecanique utilisable pour le pilotage d'un vehicule
US10101173B2 (en) * 2016-07-15 2018-10-16 The Boeing Company System and method for dynamically determining and indicating an aircraft bank limit on an aircraft instrument panel

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2845623A (en) * 1956-01-03 1958-07-29 Sperry Rand Corp Aircraft navigation system
US3386689A (en) * 1967-02-06 1968-06-04 Sperry Rand Corp Aircraft autopilot with control wheel steering
US3521839A (en) * 1967-10-02 1970-07-28 Bendix Corp Control apparatus for aircraft
US3711042A (en) * 1970-07-13 1973-01-16 Na Sa Aircraft control system
US3848833A (en) * 1972-07-14 1974-11-19 Sperry Rand Corp Aircraft automatic flight control system
US3920966A (en) * 1974-04-29 1975-11-18 Us Air Force Blended manual-automatic control system

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2262725A (en) * 1991-12-27 1993-06-30 Keith Trevor Lawes Externally referenced rotary wing cyclic pitch control.
GB2262725B (en) * 1991-12-27 1995-10-18 Keith Trevor Lawes Externally referenced rotary wing cyclic pitch control
US11679865B2 (en) 2021-06-21 2023-06-20 Honeywell International Inc. Aircraft yoke interference detection system and method

Also Published As

Publication number Publication date
IT1079172B (it) 1985-05-08
IL51185A (en) 1981-03-31
IL51185A0 (en) 1980-06-30
FR2340589A1 (fr) 1977-09-02
DE2701564A1 (de) 1977-08-04
FR2340589B1 (ja) 1982-07-23
JPS5288999A (en) 1977-07-26

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Legal Events

Date Code Title Description
PS Patent sealed [section 19, patents act 1949]
PE20 Patent expired after termination of 20 years

Effective date: 19970112