GB548195A - Improvements in and relating to automatic pilots for aircraft - Google Patents
Improvements in and relating to automatic pilots for aircraftInfo
- Publication number
- GB548195A GB548195A GB1006/41A GB100641A GB548195A GB 548195 A GB548195 A GB 548195A GB 1006/41 A GB1006/41 A GB 1006/41A GB 100641 A GB100641 A GB 100641A GB 548195 A GB548195 A GB 548195A
- Authority
- GB
- United Kingdom
- Prior art keywords
- aircraft
- slip
- course
- pendulum
- eliminate
- 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
Classifications
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
- G01C19/00—Gyroscopes; Turn-sensitive devices using vibrating masses; Turn-sensitive devices without moving masses; Measuring angular rate using gyroscopic effects
Landscapes
- Physics & Mathematics (AREA)
- Engineering & Computer Science (AREA)
- General Physics & Mathematics (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Toys (AREA)
Abstract
548,195. Automatic control systems for aircraft. SPERRY GYROSCOPE CO., Inc. March 13, 1940, No. 1006/41. Convention date March 18, 1939. Divided out of 548,190. [Class 38 (iv)] Altitude ; steering. An automatic pilot comprises means responsive to side slip, such as a pendulum, adapted to control the rate of turning affected by continuous change of setting of a course controller acting on the rudder thereby to eliminate the slip, e.g., during a banked turn. A turn may be initiated by adjustment of a knob 48 whereby the base of a gyro-vertical is tilted about the longitudinal axis of an aircraft to cause an electromagnetic pick-off 191 to adjust the ailerons to bank the craft. A pendulum 52 operates upon reversed fields of a motor 56 to adjust a potentiometer contact 58 whereby a motor 60 adjusting the setting of a course directing gyroscope is driven in the direction and at the speed required to maintain the rate of change of course necessary to eliminate any slip. Specifications 360,428, 417,995, [Group XXXVII], 492,670 and 548,190 are referred to.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US548195XA | 1939-03-18 | 1939-03-18 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB548195A true GB548195A (en) | 1942-09-30 |
Family
ID=21993729
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1006/41A Expired GB548195A (en) | 1939-03-18 | 1940-03-13 | Improvements in and relating to automatic pilots for aircraft |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB548195A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN115390590A (en) * | 2022-10-27 | 2022-11-25 | 中南大学 | Large maneuvering control method and related equipment for axisymmetric aircraft |
-
1940
- 1940-03-13 GB GB1006/41A patent/GB548195A/en not_active Expired
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN115390590A (en) * | 2022-10-27 | 2022-11-25 | 中南大学 | Large maneuvering control method and related equipment for axisymmetric aircraft |
CN115390590B (en) * | 2022-10-27 | 2023-02-28 | 中南大学 | Large maneuvering control method and related equipment for axisymmetric aircraft |
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