GB577674A - Improvements in radiolocation systems - Google Patents

Improvements in radiolocation systems

Info

Publication number
GB577674A
GB577674A GB10654/43A GB1065443A GB577674A GB 577674 A GB577674 A GB 577674A GB 10654/43 A GB10654/43 A GB 10654/43A GB 1065443 A GB1065443 A GB 1065443A GB 577674 A GB577674 A GB 577674A
Authority
GB
United Kingdom
Prior art keywords
frequency
dipoles
tube
spacing
oscillator
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
GB10654/43A
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.)
BAE Systems Aerospace Inc
Original Assignee
Hazeltine 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 Hazeltine Corp filed Critical Hazeltine Corp
Publication of GB577674A publication Critical patent/GB577674A/en
Expired legal-status Critical Current

Links

Classifications

    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q3/00Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system
    • H01Q3/22Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system varying the orientation in accordance with variation of frequency of radiated wave

Landscapes

  • Radar Systems Or Details Thereof (AREA)

Abstract

577,674. Radiolocation. HAZELTINE CORPORATION. June 6, 1942, No. 10654/43. Convention date, May 26, 1941. Divided out of 577,672. [Class 40 (v)] [Also in Group XXXVI] A system for locating objects by the reflection from them of wave signals radiated in a scanned beam comprises a number of signal radiators physically spaced in one dimension by predetermined wavelength values, means for supplying them with signals of cyclicallyvarying frequency through wave-delay means which provide an electrical spacing between adjacent radiators of a higher order of magnitude (say 5 to 50 times) than that of the physical spacing, thereby producing a sharplydirective beam, the direction of which varies cyclically with the wavelength, and means for receiving the reflected energy and using it to determine the direction of the reflector. Fig. 1 shows a transmitter providing a beam with scanning movements in mutually perpendicular planes, comprising four sets each of six dipole aerials arranged in one horizontal plane and adapted, when all are energized in the same phase, collectively to emit a sharplydefined beam in a direction perpendicular to this plane. The geometrical spacing of the dipoles of each set, and the spacing of the sets, are preferably approximately half a wavelength; 'whilst the electrical spacing of the dipoles of a set, introduced by delay networks F between them is an integral number, for example five to ten, of wavelengths. Beneath each dipole'is a reflector 17 to suppress downward radiation. Each set of dipoles is energized from a high-frequency oscillator 11 by way of a corresponding phase shifter 12a to 12d connected by a transformer to the oscillator. The magnitude of the phase shift produced by each phase shifter is controlled by a potential derived from a potential divider 9 across the output of a field-frequency generator 15, which is preferably of a saw-tooth wave-form and is controlled by a timer 14. The phases of the oscillations supplied to the sets of dipoles are thereby varied relatively to one another at a frequency of, for example, 10 to 30 cycles, so as to cause a corresponding variation in the direction of the emitted beam in a plane perpendicular to the lines in which the sets of dipoles extend. To produce a tilting movement of the beam for scanning in a perpendicular plane, a line-frequency generator 13, under control of the timer 14, causes a frequency-variation of the output of the oscillator 11, at a frequency of, for example, 500 to 5000 cycles. This causes the delay-networks F between the dipoles of each set to vary the relative phases of the energy supplied to the dipoles, causing a scanning movement of the beam in a plane parallel to the direction of each set. Fig. 2 shows a radiolocation system including the transmitter of Fig. 1 and embodying a cathode-ray indicator 24, the beam of which is scanned synchronously with the beam radiated from the aerial system by deflecting plates connected respectively to the line and field frequency generators 13, 15. Reception of a reflected wave by a non-directional antenna 22, 23 causes a receiver 21 to overcome the normal cut-off bias on the tube 24, so that a spot appears on the screen at a point indicating the direction of the reflecting object. A distance indicator 36 is operated by means involving a comparison of the frequency of the received signals and those emitted at the same moment from the oscillator 11, the signals being supplied to a modulator 32 and the difference frequency being applied to a network 35 which supplies a current of corresponding amplitude to the distance indicator. To enable a single distance indication corresponding to one of a number of reflecting objects to be obtained, the indicator 36 is rendered inoperative by a cut-off bias until supplied with a signal received by way of a differentiating circuit 44 and amplifier 43 from a photo-electric cell 40 which can be moved so as to be energized by any one of the direction-indicating spots on the screen of the tube 24. To compensate the indications on the screen of tube 24 for the delay between the emission of a signal and its reception after reflection, a signal developed by the frequency detector 35 across a resistance 30 is applied to deflecting plates 26, 27 to correct the linescanning of the tube so that it agrees with that of the generator 13 at the moment of emission of the signal. In a modified circuit, one pair of deflection plates of the tube 24 is coupled to the output of the network 35, while the other pair may be connected by a switch alternatively to the line or field scanning generator, whereby traces are obtained, the horizontal positions of which represent the co-ordinates of the position of the object, whilst the height of the trace indicates its distance. The non-directional receiving antenna may be replaced by a directional system similar to that shown in Fig. 1, the phase-shifters of the transmitting and receiving systems being synchronously controlled. Specification 577,672 is referred to.
GB10654/43A 1941-05-26 1942-06-06 Improvements in radiolocation systems Expired GB577674A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US577674XA 1941-05-26 1941-05-26

Publications (1)

Publication Number Publication Date
GB577674A true GB577674A (en) 1946-05-28

Family

ID=22012631

Family Applications (1)

Application Number Title Priority Date Filing Date
GB10654/43A Expired GB577674A (en) 1941-05-26 1942-06-06 Improvements in radiolocation systems

Country Status (1)

Country Link
GB (1) GB577674A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2072030A1 (en) * 1969-12-23 1971-09-24 Siemens Ag

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2072030A1 (en) * 1969-12-23 1971-09-24 Siemens Ag

Similar Documents

Publication Publication Date Title
US2433804A (en) Frequency-modulated pulse radio locating system
US2415094A (en) Radio measurement of distances and velocities
US2585855A (en) Radar ground-controlled approach system for aircraft
US3221328A (en) Sum-difference direction-finding device
US2403728A (en) System for indicating the position in space of an object
US2407169A (en) System for locating radiated-signal reflectors
US2929059A (en) Radio antennae systems
US2116667A (en) Radio beacon and blind landing system
US2515332A (en) Object locating system
US3107351A (en) Radar resolutions
US2403622A (en) Obstacle detecting system
US3017630A (en) Radar scanning system
US1979225A (en) Means and method of measuring distance
US2537102A (en) Radio system for identifying friendly aircraft and the like
US2682048A (en) Radio object detection apparatus
US2403278A (en) Cathode-ray sweep circuit
US2508400A (en) Frequency-modulated direction- and range-finding apparatus
US3878523A (en) Generation of scanning radio beams
US2523455A (en) Object locating system
US2510692A (en) Direction finding system
US3290685A (en) Omni-range doppler beacons and direction finding systems
GB577674A (en) Improvements in radiolocation systems
US3626419A (en) Doppler navigation system
US3409890A (en) Landing system for aircraft
GB1105758A (en) Short-range radar system