GB1173554A - Improvements in and relating to Servomechanism Systems. - Google Patents
Improvements in and relating to Servomechanism Systems.Info
- Publication number
- GB1173554A GB1173554A GB06762/68A GB1676268A GB1173554A GB 1173554 A GB1173554 A GB 1173554A GB 06762/68 A GB06762/68 A GB 06762/68A GB 1676268 A GB1676268 A GB 1676268A GB 1173554 A GB1173554 A GB 1173554A
- Authority
- GB
- United Kingdom
- Prior art keywords
- channels
- signals
- relay
- servomotors
- generators
- 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
- 238000006880 cross-coupling reaction Methods 0.000 abstract 1
- 238000001514 detection method 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
- G05D1/0077—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots with safety arrangements using redundant signals or controls
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)
- Safety Devices In Control Systems (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US63029867A | 1967-04-12 | 1967-04-12 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB1173554A true GB1173554A (en) | 1969-12-10 |
Family
ID=24526611
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB06762/68A Expired GB1173554A (en) | 1967-04-12 | 1968-04-08 | Improvements in and relating to Servomechanism Systems. |
Country Status (3)
| Country | Link |
|---|---|
| US (1) | US3462662A (enExample) |
| FR (1) | FR1562444A (enExample) |
| GB (1) | GB1173554A (enExample) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110745255A (zh) * | 2019-10-25 | 2020-02-04 | 中国航空工业集团公司沈阳飞机设计研究所 | 一种飞机伺服作动系统开车前自检方法 |
Families Citing this family (12)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3679956A (en) * | 1970-02-02 | 1972-07-25 | Ltv Electrosystems Inc | Multiple servomotor actuator |
| US3633087A (en) * | 1970-03-16 | 1972-01-04 | Rohr Corp | Electronic tracer method and apparatus for monitoring the path of a numerically controlled machine |
| US3688099A (en) * | 1971-04-28 | 1972-08-29 | Lear Siegler Inc | Automatic control system with a digital computer |
| GB1481409A (en) * | 1973-10-18 | 1977-07-27 | British Petroleum Co | Monitor systems |
| US4035705A (en) * | 1975-03-17 | 1977-07-12 | Sperry Rand Corporation | Fail-safe dual channel automatic pilot with maneuver limiting |
| US4094481A (en) * | 1977-06-30 | 1978-06-13 | Sperry Rand Corporation | Fail passive dual servo with continuous motor speed and acceleration and monitoring |
| FR2468936A1 (fr) * | 1979-11-06 | 1981-05-08 | Sfim | Dispositif pour transformer une tension electrique en un deplacement et application au pilotage automatique |
| JPH0340401B2 (enExample) * | 1980-09-30 | 1991-06-18 | ||
| US4527242A (en) * | 1982-06-28 | 1985-07-02 | Rockwell International Corporation | Automatic flight control pilot assist system |
| US4826110A (en) * | 1987-06-22 | 1989-05-02 | The Boeing Company | Oscillatory failure monitor |
| US7799273B2 (en) | 2004-05-06 | 2010-09-21 | Smp Logic Systems Llc | Manufacturing execution system for validation, quality and risk assessment and monitoring of pharmaceutical manufacturing processes |
| US8387922B2 (en) * | 2006-09-15 | 2013-03-05 | Airbus Operations Gmbh | Aerodynamic element and wing with aerodynamic element, actuator-activation module, computer, computer program and method of influencing wake eddies |
Family Cites Families (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2768343A (en) * | 1952-09-12 | 1956-10-23 | Honeywell Regulator Co | Angular velocity control device for aircraft |
| US3166691A (en) * | 1962-03-23 | 1965-01-19 | Mcgee Newman | Phase error correction circuit |
| US3135485A (en) * | 1962-06-20 | 1964-06-02 | Sperry Rand Corp | Monitoring apparatus for control systems |
-
1967
- 1967-04-12 US US630298A patent/US3462662A/en not_active Expired - Lifetime
-
1968
- 1968-04-08 GB GB06762/68A patent/GB1173554A/en not_active Expired
- 1968-04-12 FR FR1562444D patent/FR1562444A/fr not_active Expired
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110745255A (zh) * | 2019-10-25 | 2020-02-04 | 中国航空工业集团公司沈阳飞机设计研究所 | 一种飞机伺服作动系统开车前自检方法 |
Also Published As
| Publication number | Publication date |
|---|---|
| US3462662A (en) | 1969-08-19 |
| FR1562444A (enExample) | 1969-04-04 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| GB1173554A (en) | Improvements in and relating to Servomechanism Systems. | |
| US4159444A (en) | Fail operational dual electromechanical servo actuator for aircraft with model monitoring | |
| EP0321758B1 (en) | Electro-hydraulic actuator system | |
| GB1327300A (en) | Multiple channel redundant control system | |
| US3095784A (en) | Electro-hydraulic control servomechanisms | |
| US4094481A (en) | Fail passive dual servo with continuous motor speed and acceleration and monitoring | |
| US3124041A (en) | Servo amplifier | |
| US4398242A (en) | Electronic controller | |
| US2446149A (en) | Aircraft control system | |
| GB1517656A (en) | Fluid system of a work vehicle having fluid combining means and signal combining means | |
| US3269676A (en) | Valve actuator apparatus | |
| US3100861A (en) | Fail-safe control systems for aircraft | |
| GB1131669A (en) | Redundant control system | |
| GB1249658A (en) | Improvements in or relating to servo-control systems, especially for aircraft controls | |
| US3440504A (en) | Monitoring control for a servomechanism including a deadband | |
| GB1152771A (en) | Hydraeric Control System | |
| US3351315A (en) | Control apparatus | |
| GB1221451A (en) | An actuator for operating aerodynamic devices, more especially spoilers, in aircraft | |
| US3663879A (en) | Circuit for determining defective control circuits in a plural circuit flight control system | |
| US3219295A (en) | Triple safety control system | |
| GB1256123A (en) | Return pressure compensated hydraeric signal comparator | |
| GB1408126A (en) | Arrangement for monitoring and controlling a redundant hydraulic adjusting drive | |
| GB1182268A (en) | Improvements in or relating to Aircraft Control Systems. | |
| US3125712A (en) | Uator | |
| GB897627A (en) | Control apparatus for aircraft |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PS | Patent sealed [section 19, patents act 1949] | ||
| PLNP | Patent lapsed through nonpayment of renewal fees |