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GB755886A - Improvements in or relating to direction finding systems - Google Patents

Improvements in or relating to direction finding systems

Info

Publication number
GB755886A
GB755886A GB13449/54A GB1344954A GB755886A GB 755886 A GB755886 A GB 755886A GB 13449/54 A GB13449/54 A GB 13449/54A GB 1344954 A GB1344954 A GB 1344954A GB 755886 A GB755886 A GB 755886A
Authority
GB
United Kingdom
Prior art keywords
transmitter
differences
aerial
receiver
zones
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
GB13449/54A
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.)
Thales SA
Original Assignee
CSF Compagnie Generale de Telegraphie sans Fil SA
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 CSF Compagnie Generale de Telegraphie sans Fil SA filed Critical CSF Compagnie Generale de Telegraphie sans Fil SA
Publication of GB755886A publication Critical patent/GB755886A/en
Expired legal-status Critical Current

Links

Classifications

    • 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
    • G01S1/00Beacons or beacon systems transmitting signals having a characteristic or characteristics capable of being detected by non-directional receivers and defining directions, positions, or position lines fixed relatively to the beacon transmitters; Receivers co-operating therewith
    • G01S1/02Beacons or beacon systems transmitting signals having a characteristic or characteristics capable of being detected by non-directional receivers and defining directions, positions, or position lines fixed relatively to the beacon transmitters; Receivers co-operating therewith using radio waves

Landscapes

  • Engineering & Computer Science (AREA)
  • Computer Networks & Wireless Communication (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Optical Communication System (AREA)
  • Eye Examination Apparatus (AREA)

Abstract

755,886. Radio navigation. COMPAGNIE GENERALE DE TELEGRAPHIE SANS FIL. May 7, 1954 [May 7, 1953], No. 13449/54. Class 40 (7). In a system for determining the direction of a body M shown in a plan view in Fig. 1 with respect to a fixed point O, a directive transmitter beam located at the point executes a conical scan whilst the transmitter is controlled so as to emit a constant frequency carrier pulse modulated at F1, F2, F3 and F4 as the beam scans in succession each of four zones defined by two planes OP1, OP2 cutting at right angles along the axis of the cone. In a receiver carried by the body the signals D1, D2, D3 and D4 received respectively at each of said frequencies are integrated and then compared to derive the differences D1-D3 and D2-D4. These differences are proportional respectively to the rectangular co-ordinates of the displacement OM of the body from the core axis O in terms of axis OX, OY, bisecting to four zones. Fig. 4 shows one embodiment of the transmitter in which an offset aerial 10 is rotated in the focal plane of a paraboloid 11 under the control of motor 13 and is energized by a transmitter 14 operating at a constant radio frequency. The transmitter is pulse modulated by a modulator 16 under the control of a switching device 17 synchronized with the aerial scan by a drive from motor 13. Switching device 17 comprises a disc 18, Fig. 6, which is rotated between a light source and photo-cell and is formed around its periphery with serrations 25 of constant width but different spacing in the four quadrants whereby the transmitter is modulated with a different frequency in each of the four zones successively scanned by aerial 10. In the receiver, Fig. 7, the four frequencies are separated by filters 43-46 and applied to rectifiers 47-50 which integrate the corresponding signals D1-D4 and apply them to comparison devices 51. and 52. to derive the differences D1-D3 and D2-D4. The input of the receiver is a crystal rectifier 39 which feeds an amplifier 40 provided with an A.V.C. system 12, 41.
GB13449/54A 1953-05-07 1954-05-07 Improvements in or relating to direction finding systems Expired GB755886A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR755886X 1953-05-07

Publications (1)

Publication Number Publication Date
GB755886A true GB755886A (en) 1956-08-29

Family

ID=9165281

Family Applications (1)

Application Number Title Priority Date Filing Date
GB13449/54A Expired GB755886A (en) 1953-05-07 1954-05-07 Improvements in or relating to direction finding systems

Country Status (2)

Country Link
DE (1) DE961445C (en)
GB (1) GB755886A (en)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4298874A (en) 1977-01-17 1981-11-03 The Austin Company Method and apparatus for tracking objects
US4314251A (en) 1979-07-30 1982-02-02 The Austin Company Remote object position and orientation locater
US4328548A (en) 1980-04-04 1982-05-04 The Austin Company Locator for source of electromagnetic radiation having unknown structure or orientation
US4346384A (en) 1980-06-30 1982-08-24 The Austin Company Remote object position and orientation locator
US4737794A (en) * 1985-12-09 1988-04-12 Mcdonnell Douglas Corporation Method and apparatus for determining remote object orientation and position
US4742356A (en) * 1985-12-09 1988-05-03 Mcdonnell Douglas Corporation Method and apparatus for determining remote object orientation and position

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE607967C (en) * 1932-11-29 1935-01-12 Telefunken Gmbh System for the management of aircraft along a line

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4298874A (en) 1977-01-17 1981-11-03 The Austin Company Method and apparatus for tracking objects
US4314251A (en) 1979-07-30 1982-02-02 The Austin Company Remote object position and orientation locater
US4328548A (en) 1980-04-04 1982-05-04 The Austin Company Locator for source of electromagnetic radiation having unknown structure or orientation
US4346384A (en) 1980-06-30 1982-08-24 The Austin Company Remote object position and orientation locator
US4737794A (en) * 1985-12-09 1988-04-12 Mcdonnell Douglas Corporation Method and apparatus for determining remote object orientation and position
US4742356A (en) * 1985-12-09 1988-05-03 Mcdonnell Douglas Corporation Method and apparatus for determining remote object orientation and position

Also Published As

Publication number Publication date
DE961445C (en) 1957-04-04

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