GB993137A - Improvements in or modifications of control systems using servo-motors - Google Patents
Improvements in or modifications of control systems using servo-motorsInfo
- Publication number
- GB993137A GB993137A GB2484/62A GB248462A GB993137A GB 993137 A GB993137 A GB 993137A GB 2484/62 A GB2484/62 A GB 2484/62A GB 248462 A GB248462 A GB 248462A GB 993137 A GB993137 A GB 993137A
- Authority
- GB
- United Kingdom
- Prior art keywords
- servo
- automatic
- motors
- modifications
- jan
- 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
- 230000004048 modification Effects 0.000 title 1
- 238000012986 modification Methods 0.000 title 1
- 230000001133 acceleration Effects 0.000 abstract 1
- 230000001419 dependent effect Effects 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)
- Control Of Velocity Or Acceleration (AREA)
- Feedback Control In General (AREA)
Abstract
993,137. Automatic pilots. BODENSEEWERK PERKIN-ELMER & CO. G.m.b.H. Jan. 23, 1962 [Jan. 27,1961], No. 2484/62. Addition to 924,216. Heading G3R. In an automatic control system such as an automatic pilot, first and second differential components are added to the error signal and the resultant applied through an amplitude limiter to control a servo system which has a suitably chosen moment of inertia and produces feedback signals dependent on position and speed. The arrangement is designed to produce stable operation without the necessity for the acceleration feedback of the parent Specification.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DEB61022A DE1131513B (en) | 1961-01-27 | 1961-01-27 | Device for the compensation of disturbances in servomotors of flight control systems |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB993137A true GB993137A (en) | 1965-05-26 |
Family
ID=6973051
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB2484/62A Expired GB993137A (en) | 1961-01-27 | 1962-01-23 | Improvements in or modifications of control systems using servo-motors |
Country Status (2)
| Country | Link |
|---|---|
| DE (1) | DE1131513B (en) |
| GB (1) | GB993137A (en) |
-
1961
- 1961-01-27 DE DEB61022A patent/DE1131513B/en active Pending
-
1962
- 1962-01-23 GB GB2484/62A patent/GB993137A/en not_active Expired
Also Published As
| Publication number | Publication date |
|---|---|
| DE1131513B (en) | 1962-06-14 |
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