GB1520391A - Method and apparatus for automatic heading control - Google Patents
Method and apparatus for automatic heading controlInfo
- 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
Links
- 230000003111 delayed effect Effects 0.000 abstract 1
- 238000005516 engineering process Methods 0.000 abstract 1
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)
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 (de) |
DE (1) | DE2701564A1 (de) |
FR (1) | FR2340589A1 (de) |
GB (1) | GB1520391A (de) |
IL (1) | IL51185A (de) |
IT (1) | IT1079172B (de) |
Cited By (2)
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)
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)
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 |
-
1976
- 1976-12-29 IL IL51185A patent/IL51185A/xx unknown
-
1977
- 1977-01-13 GB GB1326/77A patent/GB1520391A/en not_active Expired
- 1977-01-14 IT IT19318/77A patent/IT1079172B/it active
- 1977-01-14 JP JP348177A patent/JPS5288999A/ja active Pending
- 1977-01-14 FR FR7700998A patent/FR2340589A1/fr active Granted
- 1977-01-15 DE DE19772701564 patent/DE2701564A1/de not_active Ceased
Cited By (3)
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 |
---|---|
FR2340589A1 (fr) | 1977-09-02 |
IL51185A (en) | 1981-03-31 |
DE2701564A1 (de) | 1977-08-04 |
FR2340589B1 (de) | 1982-07-23 |
JPS5288999A (en) | 1977-07-26 |
IT1079172B (it) | 1985-05-08 |
IL51185A0 (en) | 1980-06-30 |
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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 |