GB591322A - Improvements in navigating apparatus - Google Patents
Improvements in navigating apparatusInfo
- Publication number
- GB591322A GB591322A GB1237045A GB1237045A GB591322A GB 591322 A GB591322 A GB 591322A GB 1237045 A GB1237045 A GB 1237045A GB 1237045 A GB1237045 A GB 1237045A GB 591322 A GB591322 A GB 591322A
- Authority
- GB
- United Kingdom
- Prior art keywords
- craft
- display
- time base
- aerial
- orientation
- 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
- 241001646071 Prioneris Species 0.000 abstract 2
- 230000001360 synchronised Effects 0.000 abstract 2
- 230000004048 modification Effects 0.000 abstract 1
- 238000006011 modification reaction Methods 0.000 abstract 1
- 238000004804 winding Methods 0.000 abstract 1
Classifications
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
- G01S7/00—Details of systems according to groups G01S13/00, G01S15/00, G01S17/00
- G01S7/02—Details of systems according to groups G01S13/00, G01S15/00, G01S17/00 of systems according to group G01S13/00
- G01S7/04—Display arrangements
- G01S7/06—Cathode-ray tube displays or other two dimensional or three-dimensional displays
- G01S7/24—Cathode-ray tube displays or other two dimensional or three-dimensional displays the display being orientated or displaced in accordance with movement of object carrying the transmitting and receiving apparatus, e.g. true-motion radar
Landscapes
- Engineering & Computer Science (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Computer Networks & Wireless Communication (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Radar Systems Or Details Thereof (AREA)
Abstract
591,322. Radiolocation. O'KANE, B. J., and DICKIE, E. J. May 16, 1945, No. 12370. [Class 40 (v)] In a pulse radar system with a P.P.I. display for use on a moving craft or vehicle, means are provided for controlling the rotation of the time base so as to maintain the orientation of the display with reference to some bearing other than the instantaneous course bearing, e.g. true or magnetic north or the track of the craft. As shown in the Figure, a saw-tooth time-base voltage from the generator 8 is applied to the rotor winding 9 of a rotary transformer and the outputs from the two perpendicular stator windings are applied to the. perpendicular deflection systems of the cathode-ray tube 7, the rotor 9 being mounted on the same shaft 3 as the aerial 1 so that rotation of the aerial by the motor 6 causes a synchronous rotation of the radial time base 15. The time base is initially set up so that the top of the P.P.I. display represents true north and in order to compensate for changes in the orientation of the craft the stator windings are mounted on a rotatable frame 10 geared to a repeater motor 20, which is connected to a distant reading compass 21. Alternatively, if it is desired to orientate the display in relation to the track of the craft the navigational instrument may comprise a drift angle computer. In a modification, Fig. 2 (not shown), the radial time base is produced by a rotary potentiometer having two 90 degree displaced wipers the voltage outputs from which are proportional to the sine and cosine of the angular position of the spindle and are applied to control the amplitudes of two sets of synchronous square waves which are applied through R.C. saw-tooth generating circuits . to the X and Y plates of the cathode-ray tube. The orientation compensation is obtained by gearing the aerial shaft and the navigational repeater motor to the two sun wheels of a differential gear, the potentiometer spindle being geared to the planet wheel. Alternatively, the rotary potentiometer could be replaced by the rotary transformer of Fig. 1 with fixed stators or the compensation system of Fig. I could be applied to the rotary potentiometer.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US763568A US2731633A (en) | 1945-05-16 | 1947-07-25 | Azimuth stabilized plan position indicator |
Publications (1)
Publication Number | Publication Date |
---|---|
GB591322A true GB591322A (en) | 1947-08-14 |
Family
ID=1717800
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1237045A Expired GB591322A (en) | 1945-05-16 | 1945-05-16 | Improvements in navigating apparatus |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB591322A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2688130A (en) * | 1954-08-31 | Radar pilot | ||
US2697827A (en) * | 1948-08-06 | 1954-12-21 | Sperry Corp | Combined p. p. i. presentation |
US2727229A (en) * | 1950-08-07 | 1955-12-13 | James L Anast | Radar navigational system for aircraft |
-
1945
- 1945-05-16 GB GB1237045A patent/GB591322A/en not_active Expired
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2688130A (en) * | 1954-08-31 | Radar pilot | ||
US2697827A (en) * | 1948-08-06 | 1954-12-21 | Sperry Corp | Combined p. p. i. presentation |
US2727229A (en) * | 1950-08-07 | 1955-12-13 | James L Anast | Radar navigational system for aircraft |
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