GB841816A - "servo system" - Google Patents
"servo system"Info
- Publication number
- GB841816A GB841816A GB2130/59A GB213059A GB841816A GB 841816 A GB841816 A GB 841816A GB 2130/59 A GB2130/59 A GB 2130/59A GB 213059 A GB213059 A GB 213059A GB 841816 A GB841816 A GB 841816A
- Authority
- GB
- United Kingdom
- Prior art keywords
- jan
- group xxxv
- servo system
- adjustable
- constant
- 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
- 230000003321 amplification Effects 0.000 abstract 1
- 238000003199 nucleic acid amplification 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
- G05D1/0066—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots with safety arrangements for limitation of acceleration or stress
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 Amplification And Gain Control (AREA)
- Amplifiers (AREA)
Abstract
841,816. Limiting circuits. BENDIX AVIATION CORPORATION. Jan. 20, 1959 [Jan. 28, 1958], No. 2130/59. Class 40(6). [Also in Group XXXV] A network of constant amplification but adjustable maximum output comprises an amplifier 2 with a power output stage 3 followed by an adjustable attenuator 5, the gain being maintained constant by an overall negative feedback path 7. The arrangement is described as applied to a servo control system (see Group XXXV).
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US841816XA | 1958-01-28 | 1958-01-28 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB841816A true GB841816A (en) | 1960-07-20 |
Family
ID=22183352
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB2130/59A Expired GB841816A (en) | 1958-01-28 | 1959-01-20 | "servo system" |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB841816A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0122159A2 (en) * | 1983-04-12 | 1984-10-17 | Niigata Engineering Co., Ltd. | System for controlling rotation of rotary mechanism in Z-type propulsion apparatus |
EP0143851A1 (en) * | 1983-03-30 | 1985-06-12 | Niigata Engineering Co., Ltd. | Turning controller for z-type propulsion device |
-
1959
- 1959-01-20 GB GB2130/59A patent/GB841816A/en not_active Expired
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0143851A1 (en) * | 1983-03-30 | 1985-06-12 | Niigata Engineering Co., Ltd. | Turning controller for z-type propulsion device |
EP0143851A4 (en) * | 1983-03-30 | 1987-10-22 | Niigata Engineering Co Ltd | Turning controller for z-type propulsion device. |
EP0122159A2 (en) * | 1983-04-12 | 1984-10-17 | Niigata Engineering Co., Ltd. | System for controlling rotation of rotary mechanism in Z-type propulsion apparatus |
EP0122159A3 (en) * | 1983-04-12 | 1988-01-20 | Niigata Engineering Co., Ltd. | System for controlling rotation of rotary mechanism in z-type propulsion apparatus |
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