GB743663A - Noise eliminator for automatic pilot systems - Google Patents
Noise eliminator for automatic pilot systemsInfo
- Publication number
- GB743663A GB743663A GB3744/53A GB374453A GB743663A GB 743663 A GB743663 A GB 743663A GB 3744/53 A GB3744/53 A GB 3744/53A GB 374453 A GB374453 A GB 374453A GB 743663 A GB743663 A GB 743663A
- Authority
- GB
- United Kingdom
- Prior art keywords
- amplifier
- pick
- automatic pilot
- noise eliminator
- pilot 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
- 230000001939 inductive effect Effects 0.000 abstract 1
- 238000002347 injection Methods 0.000 abstract 1
- 239000007924 injection Substances 0.000 abstract 1
- 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
- G05D1/0055—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 Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
- Variable-Direction Aerials And Aerial Arrays (AREA)
Abstract
743,663. Automatic steering control systems. BENDIX AVIATION CORPORATION. Feb. 10, 1953 [April 4, 1952], No. 3744/53. Class 38 (4). In an automatic aircraft pilot an elevator 12 is adjusted by a servomotor 10 controlled through a thermionic valve amplifier 44 in known manner. To reduce noise injection into the input of amplifier 44, the A.C. outputs from the pick-off of a gyro 50, the pick-off of an altimeter 100, a position feed-back inductive device 140, and a rate feed-back generator 150, are applied to amplifier 44 through twisted pairs of leads 90, 130, 149, 152 and transformers 200, 211, 223, 235 respectively, the latter having earthed centre-tapped primary windings. Specifications 662,831 and 662,918 are referred to.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US743663XA | 1952-04-04 | 1952-04-04 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB743663A true GB743663A (en) | 1956-01-18 |
Family
ID=22119166
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB3744/53A Expired GB743663A (en) | 1952-04-04 | 1953-02-10 | Noise eliminator for automatic pilot systems |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB743663A (en) |
-
1953
- 1953-02-10 GB GB3744/53A patent/GB743663A/en not_active Expired
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