GB625917A - Improvements in or relating to navigation devices - Google Patents
Improvements in or relating to navigation devicesInfo
- Publication number
- GB625917A GB625917A GB29834/46A GB2983446A GB625917A GB 625917 A GB625917 A GB 625917A GB 29834/46 A GB29834/46 A GB 29834/46A GB 2983446 A GB2983446 A GB 2983446A GB 625917 A GB625917 A GB 625917A
- Authority
- GB
- United Kingdom
- Prior art keywords
- displacement
- signals
- valves
- condensers
- craft
- 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 5
- 230000000295 complement effect Effects 0.000 abstract 1
- 239000002131 composite material Substances 0.000 abstract 1
- 230000008878 coupling Effects 0.000 abstract 1
- 238000010168 coupling process Methods 0.000 abstract 1
- 238000005859 coupling reaction Methods 0.000 abstract 1
- 238000010079 rubber tapping 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
- G05D1/02—Control of position or course in two dimensions
- G05D1/0202—Control of position or course in two dimensions specially adapted to aircraft
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)
- Navigation (AREA)
- Gyroscopes (AREA)
Abstract
625,917. Radio navigation. SPERRY GYROSCOPE CO., Inc. Oct. 7, 1946, No. 29834. Convention date, Aug. 7, 1943. [Class 40 (vii)] In order to enable a craft to follow an asymptotic approach to the equi-signal courseline defined by an overlapping-beam radio beacon, the receiver carried by the craft comprises an indicator responsive to both the displacement of the craft from the course-line and to the rate of change thereof, so that by maintaining the indicator at a zero indication the desired approach will be made. The beacon may radiate signals of either the complementary or simultaneous kind and may be used to define a course in either the horizontal or vertical plane. Fig. 3 illustrates a system wherein the two lobes are modulated at different audio-frequencies. The audio-frequencies are separated at the receiver, which is similar to that described in Specification 550,660 as far as the audio-frequency stage, and applied to respective transformers 12 and 13. The signals at tappings 17 and 18, whose difference is a measure of the displacement of the craft from the course, are applied to the grids of rectifying valves 19 and 21. These signals are also separately rectified by double-diode 24 and applied through differentiating condensers to the grids of valves 22 and 23 which have common cathode circuits with valves 19 and 21 respectively. The outputs from these cathode circuits are applied differentially to the meter M which consequently records a signal compounded from signals proportional to the displacement and its rate of change. The sharpness of the asymptotic approach may be controlled by adjusting the potentiometer 27 to adjust the relative amplitudes of the displacement and rate of change signals. In an alternative circuit, Fig. 4, the outputs of the transformers 12 and 13 are rectified at 33 and 34 and applied by resistors 39 and 41 respectively and condensers 42 and 43 respectively to grids of valves 38. The couplings via the resistors provide a component proportional to the displacement and those via the condensers provide a component proportional to its rate of change, so that the signal applied to the meter M is a composite signal, as before. The sharpness of the approach path may be varied by varying the resistors 39 and 41 and by switching in or out additional condensers 47 and 48.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US625917XA | 1943-08-07 | 1943-08-07 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB625917A true GB625917A (en) | 1949-07-06 |
Family
ID=22043489
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB29834/46A Expired GB625917A (en) | 1943-08-07 | 1946-10-07 | Improvements in or relating to navigation devices |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB625917A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1099361B (en) * | 1952-08-29 | 1961-02-09 | Wiesing Ab | Device for deriving control commands to bring an aircraft to a beacon |
DE1106609B (en) * | 1954-09-23 | 1961-05-10 | Sperry Rand Corp | Aircraft landing facility |
-
1946
- 1946-10-07 GB GB29834/46A patent/GB625917A/en not_active Expired
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1099361B (en) * | 1952-08-29 | 1961-02-09 | Wiesing Ab | Device for deriving control commands to bring an aircraft to a beacon |
DE1106609B (en) * | 1954-09-23 | 1961-05-10 | Sperry Rand Corp | Aircraft landing facility |
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