GB724516A - Improvements in or relating to electronic servo systems - Google Patents
Improvements in or relating to electronic servo systemsInfo
- Publication number
- GB724516A GB724516A GB12389/51A GB1238951A GB724516A GB 724516 A GB724516 A GB 724516A GB 12389/51 A GB12389/51 A GB 12389/51A GB 1238951 A GB1238951 A GB 1238951A GB 724516 A GB724516 A GB 724516A
- Authority
- GB
- United Kingdom
- Prior art keywords
- potentiometer
- signal
- servomotor
- amplifier
- pitch
- 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
- 230000001419 dependent effect Effects 0.000 abstract 2
- 238000004804 winding 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
- G05D1/08—Control of attitude, i.e. control of roll, pitch, or yaw
- G05D1/0808—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft
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)
Abstract
724,516. Automatic control systems. SPERRY GYROSCOPE CO., Ltd. May 16, 1952 [May 26, 1951], No. 12389/51. Class 38 (4). In a servo system applied to elevator control by an aircraft automatic pilot, a gyro vertical (not shown) detecting pitch is associated with a potentiometer pick-off P2, a D.C. signal from which is applied to the input terminals A, B of an electronic amplifier 7 the output of which, from the terminals C, D, controls the energization of the winding 12 of an electromagnetic slipping clutch 13 between a continuously driven member 14 and a control valve 45 controlling a hydraulic servomotor 51 correcting the position of the aircraft elevator so that pitch is maintained at a value determined by the setting of a potentiometer P3 supplying a second D.C. signal to amplifier 7 in opposition to the signal from potentiometer P2. Control valve 45 is maintained at a position corresponding to the pitch error by a D.C. follow-up signal which is derived from a potentiometer P4 associated with the control valve, and applied to the input of amplifier 7. The speed of servomotor 51 is thus dependent on the pitch error and a followup signal dependent on servomotor speed is derived through a condenser C1 from a potentiometer P5 associated with the servomotor, and applied to the input of amplifier 7. Specifications 690,982 and 718,171 are referred to.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB12389/51A GB724516A (en) | 1951-05-26 | 1951-05-26 | Improvements in or relating to electronic servo systems |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB12389/51A GB724516A (en) | 1951-05-26 | 1951-05-26 | Improvements in or relating to electronic servo systems |
Publications (1)
Publication Number | Publication Date |
---|---|
GB724516A true GB724516A (en) | 1955-02-23 |
Family
ID=10003666
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB12389/51A Expired GB724516A (en) | 1951-05-26 | 1951-05-26 | Improvements in or relating to electronic servo systems |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB724516A (en) |
-
1951
- 1951-05-26 GB GB12389/51A patent/GB724516A/en not_active Expired
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