GB698034A - Improvements in or relating to apparatus for controlling aircraft - Google Patents
Improvements in or relating to apparatus for controlling aircraftInfo
- Publication number
- GB698034A GB698034A GB29407/48A GB2940748A GB698034A GB 698034 A GB698034 A GB 698034A GB 29407/48 A GB29407/48 A GB 29407/48A GB 2940748 A GB2940748 A GB 2940748A GB 698034 A GB698034 A GB 698034A
- Authority
- GB
- United Kingdom
- Prior art keywords
- system similar
- gyro
- potentiometers
- potentiometer
- nov
- 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
- 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
- G05D1/08—Control of attitude, i.e. control of roll, pitch, or yaw
- G05D1/0808—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft
- G05D1/0816—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft to ensure stability
- G05D1/085—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft to ensure stability to ensure coordination between different movements
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 Multiple Motors (AREA)
Abstract
698,034. Automatic control systems. WESTINGHOUSE ELECTRIC INTERNATIONAL CO. Nov. 12, 1948 [Nov. 14, 1947], No. 29407/48. Drawings to Specification. Class 38 (iv). The subject-matter of this Specification is in the main identical with that of Specifications 698,033, 698,037 and 698,038, but involves, among others, the following modified arrangements : (a) A system similar to that of Specification 698,038, in which the directional gyro controls the bias of the rate-of-turn gyro instead of that of the bank gyro and the relay associated with the servomotor operating the second potentiometer. (b) A system similar to that of Specification 698,038, in which the armature of the servomotor adjusting the second potentiometer upon operation of the hand wheel is supplied directly by the voltage between the sliders of the two potentiometers. (c) A system similar to that of Specification 698,038, in which a rheostat is provided in series with each of the three outputs taken from the two potentiometers to bias the three rate gyros upon operation of the hand wheel. These rheostats may be manually adjusted to three pre-set positions or automatically controlled by an airspeed responsive diaphragm to give control surface displacements suited to airspeed. Specification 698,032 also is referred to.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US698034XA | 1947-11-14 | 1947-11-14 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB698034A true GB698034A (en) | 1953-10-07 |
Family
ID=22091311
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB29407/48A Expired GB698034A (en) | 1947-11-14 | 1948-11-12 | Improvements in or relating to apparatus for controlling aircraft |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB698034A (en) |
-
1948
- 1948-11-12 GB GB29407/48A patent/GB698034A/en not_active Expired
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