GB777730A - Improvements in or relating to safety devices for automatic pilots - Google Patents
Improvements in or relating to safety devices for automatic pilotsInfo
- Publication number
- GB777730A GB777730A GB23654/54A GB2365454A GB777730A GB 777730 A GB777730 A GB 777730A GB 23654/54 A GB23654/54 A GB 23654/54A GB 2365454 A GB2365454 A GB 2365454A GB 777730 A GB777730 A GB 777730A
- Authority
- GB
- United Kingdom
- Prior art keywords
- pitch
- difference
- elevators
- actual
- automatic pilot
- 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
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 Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
Abstract
777,730. Automatic steering control systems. SMITH & SONS (ENGLAND), Ltd., S. Aug. 8, 1955 [Aug. 13, 1954], No. 23654/54. Class 38 (4). The difference between a signal constituting the reference attitude of an aircraft automatic pilot and a signal representing actual attitude is operated on by a specified mathematical differential operator and serves to operate a warning device or disable the automatic pilot when the difference exceeds a predetermined value. The invention is applied to an aircraft automatic pilot in which deviation in rate of pitch, as detected by a gyro 1, from a desired value, set by a controller 3, results in a direct current difference signal being applied to an amplifier 6, the output of which controls a servomotor 7 adjusting elevators (not shown) to maintain the desired rate of pitch. To prevent an undesirable condition of loading of the elevators, direct current signals dependent on the set rate of pitch, from controller 3, and the actual pitch angle, as detected by a separate gyro 12, are supplied to a resistance-capacity network 10, 12 so that a signal representing the difference between the actual and desired rates of pitch operated on by the specified differential operator serves, through a potentiometer 15 automatically adjusted in accordance with airspeed, to operate a warning device 17 or declutch servomotor 7 from the elevators when the difference exceeds a predetermined value.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB23654/54A GB777730A (en) | 1954-08-13 | 1954-08-13 | Improvements in or relating to safety devices for automatic pilots |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB23654/54A GB777730A (en) | 1954-08-13 | 1954-08-13 | Improvements in or relating to safety devices for automatic pilots |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB777730A true GB777730A (en) | 1957-06-26 |
Family
ID=10199147
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB23654/54A Expired GB777730A (en) | 1954-08-13 | 1954-08-13 | Improvements in or relating to safety devices for automatic pilots |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB777730A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE1267991B (en) * | 1958-08-15 | 1968-05-09 | Smith & Sons Ltd S | Safety device for the automatic control device of an aircraft |
-
1954
- 1954-08-13 GB GB23654/54A patent/GB777730A/en not_active Expired
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE1267991B (en) * | 1958-08-15 | 1968-05-09 | Smith & Sons Ltd S | Safety device for the automatic control device of an aircraft |
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