GB698909A - System for composite cathode ray tube indication - Google Patents

System for composite cathode ray tube indication

Info

Publication number
GB698909A
GB698909A GB13931/51A GB1393151A GB698909A GB 698909 A GB698909 A GB 698909A GB 13931/51 A GB13931/51 A GB 13931/51A GB 1393151 A GB1393151 A GB 1393151A GB 698909 A GB698909 A GB 698909A
Authority
GB
United Kingdom
Prior art keywords
display
elevation
azimuth
valves
clipping
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
Application number
GB13931/51A
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Bendix Aviation Corp
Original Assignee
Bendix Aviation Corp
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Bendix Aviation Corp filed Critical Bendix Aviation Corp
Publication of GB698909A publication Critical patent/GB698909A/en
Expired legal-status Critical Current

Links

Classifications

    • HELECTRICITY
    • H03ELECTRONIC CIRCUITRY
    • H03KPULSE TECHNIQUE
    • H03K17/00Electronic switching or gating, i.e. not by contact-making and –breaking
    • H03K17/51Electronic switching or gating, i.e. not by contact-making and –breaking characterised by the components used
    • H03K17/54Electronic switching or gating, i.e. not by contact-making and –breaking characterised by the components used by the use, as active elements of vacuum tubes
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01SRADIO 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
    • G01S7/00Details of systems according to groups G01S13/00, G01S15/00, G01S17/00
    • G01S7/02Details of systems according to groups G01S13/00, G01S15/00, G01S17/00 of systems according to group G01S13/00
    • G01S7/04Display arrangements
    • G01S7/06Cathode-ray tube displays or other two dimensional or three-dimensional displays
    • G01S7/20Stereoscopic displays; Three-dimensional displays; Pseudo-three-dimensional displays

Landscapes

  • Engineering & Computer Science (AREA)
  • Computer Networks & Wireless Communication (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Radar Systems Or Details Thereof (AREA)

Abstract

698,909. Radio-navigation, valve gating circuits. BENDIX AVIATION CORPORATION. June 12, 1951 [June 26, 1950], No. 13931/51. Classes 40 (vi) and 40 (vii). The indicator for a ground control approach radar system consists of a cathode-ray tube on which may be simultaneously made visible two presentations of sector form, one conveying elevation-range information and the other bearing-range information. Clipping means are used to prevent overlap of the two displays controlled by one of a pair of voltages each of which is a function of the scan position of the elevation and azimuth aerial systems respectively and including means generating a saw-tooth output voltage of an amplitude dependent on the amplitude of the control voltage, means to generate an energy pulse at the instant the saw-tooth exceeds a predetermined value, and the utilization of the energy pulse for blanking purposes. Fig. 3 shows the form of presentation on the screen 26 of a cathode-ray tube. The upper display with its origin at point 12 is a sector elevation range display showing glide path 14 and the lower display is an azimuth-range display with its origin at 18 and showing the approach path 20 and runway 21. The approach and glide path markings may be marked or projected on to the screen and the range marks marked or formed electronically. As shown, both displays are clipped along the parallel horizontal lines 13 and 27. In the system described a master switch unit directs alternate pulses to the elevation and azimuth antennae respectively and gates the receiver and display tube scanning circuits in synchronism so that video signals received only by the correct antenna system are displayed and only on the appropriate display. Range marks may be added to both displays. Besides this the switching unit also applies square waveform biasing voltages to the deflection coils of the display tube to alternate the origin of the display between 12 and 18 as required and renders the azimuth and elevation display clipping circuits effective in alternation. The circuit feeding azimuth and elevation scanning antenna position data alternately to the display sweep circuits comprises azimuth voltage input terminals 106 and 107 feeding respectively the grids of valves 121 and 124 and elevation voltage input terminals 113 and 114 feeding respectively the grids of valves 122 and 125. Valves 121 to 125 are cathode followers, 121 and 122 having a common cathode circuit coupled to output terminal 123 and 124 and 125 having a common cathode circuit coupled to output terminal 126. Opositely phased squarewaveforms J and K are applied to the grids of clamp valves 108, 109, and 117 and 118 to render the two pairs of valves alternately conductive and so alternately prevent the passage of azimuth and of elevation signals to the output terminals. The clipping circuit preventing the overlap of the two sector displays consists of two parts. In the first part azimuth angle voltage applied at 129, but rendered effective only during the azimuth display scans by a gate voltage applied at 156, is used to initiate the generation by relaxation oscillator 47 of a saw-tooth of an amplitude dependent of the input signal. Valve 134 conducts during the initial part of the saw-tooth and until a given amplitude is reached giving a substantially square-wave output 138 with a fixed rear edge and a front edge determined by the input. The pulse is differentiated and the front edge of the resulting waveform passed by gate valve 142 to trigger a flip-flop circuit controlling the application of blanking pulse to grid of the display tube. The second (elevation) part of the clipping circuit is of simpler form due to the clipping being along the scan line corresponding to the horizontal and consist of a flip-flop circuit 160 together with gate valves which trigger circuit 150 to produce clipping slightly delayed on the transmitted pulse for all scan angles below the horizontal. Specification 698,940 is referred to.
GB13931/51A 1950-06-26 1951-06-12 System for composite cathode ray tube indication Expired GB698909A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US170326A US2855591A (en) 1950-06-26 1950-06-26 System for generating discrete side-byside displays on a cathode ray tube

Publications (1)

Publication Number Publication Date
GB698909A true GB698909A (en) 1953-10-28

Family

ID=22619444

Family Applications (1)

Application Number Title Priority Date Filing Date
GB13931/51A Expired GB698909A (en) 1950-06-26 1951-06-12 System for composite cathode ray tube indication

Country Status (4)

Country Link
US (1) US2855591A (en)
FR (1) FR1049366A (en)
GB (1) GB698909A (en)
NL (1) NL162235B (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CA629133A (en) * 1954-10-26 1961-10-17 Arthur L. Brockway, Jr. Ground controlled approach indicator system

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2423024A (en) * 1941-12-26 1947-06-24 Rca Corp Radio pulse altimeter and object detector
US2405231A (en) * 1942-03-31 1946-08-06 Bell Telephone Labor Inc Aircraft blind landing system
US2421747A (en) * 1943-07-14 1947-06-10 Bell Telephone Labor Inc Object locating system
US2482759A (en) * 1945-04-16 1949-09-27 Jr Ralph D Goodrich Electronic switch with common cathode output
NL72116C (en) * 1945-04-17
US2541399A (en) * 1945-11-19 1951-02-13 Blake Kenneth Electronic switch
US2570251A (en) * 1946-06-08 1951-10-09 Sperry Corp Pulse echo direction and distance indicator
US2483644A (en) * 1947-01-21 1949-10-04 Gilfillan Bros Inc Electronic angle indication with particular reference to radar systems
US2649581A (en) * 1947-09-29 1953-08-18 Gilfillan Bros Inc Single scope two-coordinate radar system
US2549641A (en) * 1947-10-31 1951-04-17 Rca Corp Display of three-dimensional information
US2557085A (en) * 1948-02-27 1951-06-19 Fisk Bert Electronic switch

Also Published As

Publication number Publication date
FR1049366A (en) 1953-12-29
US2855591A (en) 1958-10-07
NL162235B (en)

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