GB1429743A - Apparatus for transmitting bearing information - Google Patents

Apparatus for transmitting bearing information

Info

Publication number
GB1429743A
GB1429743A GB1133674A GB1133674A GB1429743A GB 1429743 A GB1429743 A GB 1429743A GB 1133674 A GB1133674 A GB 1133674A GB 1133674 A GB1133674 A GB 1133674A GB 1429743 A GB1429743 A GB 1429743A
Authority
GB
United Kingdom
Prior art keywords
phase
aerial
signal
carrier frequency
aerials
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
GB1133674A
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.)
STC PLC
Original Assignee
Standard Telephone and Cables PLC
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 Standard Telephone and Cables PLC filed Critical Standard Telephone and Cables PLC
Priority to GB1133674A priority Critical patent/GB1429743A/en
Priority to GB3097875A priority patent/GB1472239A/en
Priority to GB3097775A priority patent/GB1484802A/en
Priority to GB3166375A priority patent/GB1488757A/en
Publication of GB1429743A publication Critical patent/GB1429743A/en
Priority to GB5111877A priority patent/GB1538827A/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
    • G01S1/08Systems for determining direction or position line
    • G01S1/44Rotating or oscillating beam beacons defining directions in the plane of rotation or oscillation

Landscapes

  • Engineering & Computer Science (AREA)
  • Computer Networks & Wireless Communication (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Digital Transmission Methods That Use Modulated Carrier Waves (AREA)

Abstract

1429743 Radio navigation STANDARD TELEPHONES & CABLES Ltd 14 March 1974 11336/74 Heading H4D Apparatus for transmitting bearing information comprises two fixed omnidirectional aerials A1, A2, Fig. 1, spaced a predetermined distance apart, means for transmitting from one aerial (A2) a composite signal of a VHF carrier frequency signal modulated by an audio frequency signal and the unmodulated carrier frequency signal, the said two signals being in antiphase, means for transmitting from the other aerial (A1) the modulated signal only, means for cyclically varying the relative phase between the two transmitted signals, and means for distinctively altering the audio frequency modulation of the carrier frequency signal at the commmencement of each said cyclic variation of relative phase. As described, the output from a VHF oscillator is divided by a power splitting network P and part is fed to a modulator M, where it is modulated by a audio frequency tone. The modulated carrier frequency signal is then fed to a hybrid circuit H1, where it is divided equally to feed two further hybrid circuits H2, H3. The hybrid circuit H2 also receives an unmodulated carrier frequency signal from the network P. The modulated and the unmodulated signals are combined in the hybrid circuit H2, the respective path lengths being arranged so that the two signals are in anti-phase. The outputs of the hybrid circuits H3, H2 are fed to the aerials A1, A2, which are spaced #/4 apart (#=wavelength at the carrier frequency). The path lengths H1 to A1 and H1 to A2 are arranged so that at the aerials the transmitted carrier frequency signals are initially in quadrature phase relationship, i.e., # 1 =# 2 +#/2 (# 1 =phase at the aerial A1, # 2 = phase at the aerial A2). The feed line from the hybrid circuit H3 to the aerial A1 also includes a line strecher or variable phase shifter circuit L, which varies the phase of the signal to the aerial A1 at a slow rate, e.g., over a period of one minute, under the control of a unit C. The total phase variation introduced is such that at the end of a cycle # 1 =# 2 + 3#/2. Therefore, at time t, # 1 =# 2 +#/ 2 +(t/T).# ,where T is the duration of the phase varying cycle. The control unit C is also operative upon the modulator M to key it initially with a station identification signal, e.g., a Morse code group, and thereafter, following a five to ten seconds period of uninterrupted audio frequency modulation, to key it in successive pulses of, for example, 0À9 seconds audio frequency modulation separated by 0À1 seconds intervals without modulation. A receiving station on a particular bearing from the transmitting station observes minimum modulation of the signal therefrom at a unique instant during the cycle of phase change. Hence, by counting the number of modulation pulses from the initial identification signal until that minimum, an indication of the bearing angle is obtained. In order to improve resolution three aerials may be provided at the transmitting station, which are spaced in a straight line at equal intervals of, for example, #/4. In a first cycle of transmission, the centre aerial and one outer aerial are used, followed by a second similar cycle of transmission using the outer two aerials, and so on.
GB1133674A 1974-03-14 1974-03-14 Apparatus for transmitting bearing information Expired GB1429743A (en)

Priority Applications (5)

Application Number Priority Date Filing Date Title
GB1133674A GB1429743A (en) 1974-03-14 1974-03-14 Apparatus for transmitting bearing information
GB3097875A GB1472239A (en) 1974-03-14 1975-07-24 Apparatus for transmitting bearing information
GB3097775A GB1484802A (en) 1974-03-14 1975-07-24 Apparatus for transmitting bearing information
GB3166375A GB1488757A (en) 1974-03-14 1975-07-29 Apparatus for transmitting bearing information
GB5111877A GB1538827A (en) 1974-03-14 1977-12-08 Coastal navigation aid

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1133674A GB1429743A (en) 1974-03-14 1974-03-14 Apparatus for transmitting bearing information

Publications (1)

Publication Number Publication Date
GB1429743A true GB1429743A (en) 1976-03-24

Family

ID=9984392

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1133674A Expired GB1429743A (en) 1974-03-14 1974-03-14 Apparatus for transmitting bearing information

Country Status (1)

Country Link
GB (1) GB1429743A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2017174838A1 (en) * 2016-04-08 2017-10-12 Universidad De Huelva Lighthouse identification system

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2017174838A1 (en) * 2016-04-08 2017-10-12 Universidad De Huelva Lighthouse identification system

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Legal Events

Date Code Title Description
PS Patent sealed
746 Register noted 'licences of right' (sect. 46/1977)
PCNP Patent ceased through non-payment of renewal fee