GB673379A - Safety devices for electric automatic control systems - Google Patents
Safety devices for electric automatic control systemsInfo
- Publication number
- GB673379A GB673379A GB22598/49A GB2259849A GB673379A GB 673379 A GB673379 A GB 673379A GB 22598/49 A GB22598/49 A GB 22598/49A GB 2259849 A GB2259849 A GB 2259849A GB 673379 A GB673379 A GB 673379A
- Authority
- GB
- United Kingdom
- Prior art keywords
- signal
- servomotor
- rudder
- servo
- control systems
- 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 1
- 238000006073 displacement reaction 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
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)
- Gyroscopes (AREA)
Abstract
673,379. Automatic servo control systems. SMITH & SONS (ENGLAND), Ltd., S., and FURZEHILL LABORATORIES, Ltd. Nov. 28, 1950 [Aug. 31, 1949], No. 22598/49. Class 38 (iv). In a servo control system for an automatic pilot a testing signal having a signal frequency higher than that to which the servomotor can respond (e.g. 40 c.p.s.) is injected in series with the deviation signal, and its magnitude and phase are checked at the motor terminals to detect any fault in the servo amplifier. As applied to an automatic pilot such as that described in Specification 611,037, wherein the rudder 9 is controlled by signals from a compass 2, rate of turn gyro 1, and speed of rudder displacement generator 5, a testing signal from a modulator 21 is also injected into the amplifier 3. The modulator is fed from a 400-cycle source 25 (common to the other units of the servo system) and modulated at the test frequency by an oscillator 20. The signal at the servomotor terminals is demodulated and filtered to remove any control signals, and then compared with the original test frequency in a demodulator 24 to produce a D.C. output dependent on its amplitude and phase. This output is fed to a polarized relay 17 controlling the clutch 6 between the servomotor and the rudder.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB22598/49A GB673379A (en) | 1949-08-31 | 1949-08-31 | Safety devices for electric automatic control systems |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB22598/49A GB673379A (en) | 1949-08-31 | 1949-08-31 | Safety devices for electric automatic control systems |
Publications (1)
Publication Number | Publication Date |
---|---|
GB673379A true GB673379A (en) | 1952-06-04 |
Family
ID=10182038
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB22598/49A Expired GB673379A (en) | 1949-08-31 | 1949-08-31 | Safety devices for electric automatic control systems |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB673379A (en) |
-
1949
- 1949-08-31 GB GB22598/49A patent/GB673379A/en not_active Expired
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