GB1278275A - Radio hyperbolic navigation - Google Patents

Radio hyperbolic navigation

Info

Publication number
GB1278275A
GB1278275A GB33922/69A GB3392269A GB1278275A GB 1278275 A GB1278275 A GB 1278275A GB 33922/69 A GB33922/69 A GB 33922/69A GB 3392269 A GB3392269 A GB 3392269A GB 1278275 A GB1278275 A GB 1278275A
Authority
GB
United Kingdom
Prior art keywords
phase
signals
signal
frequency
receiver
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
GB33922/69A
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.)
& D Applic Des Tech Nouvelles
Original Assignee
& D Applic Des Tech Nouvelles
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 & D Applic Des Tech Nouvelles filed Critical & D Applic Des Tech Nouvelles
Publication of GB1278275A publication Critical patent/GB1278275A/en
Expired legal-status Critical Current

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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
    • G01S1/20Systems for determining direction or position line using a comparison of transit time of synchronised signals transmitted from non-directional antennas or antenna systems spaced apart, i.e. path-difference systems
    • G01S1/30Systems for determining direction or position line using a comparison of transit time of synchronised signals transmitted from non-directional antennas or antenna systems spaced apart, i.e. path-difference systems the synchronised signals being continuous waves or intermittent trains of continuous waves, the intermittency not being for the purpose of determining direction or position line and the transit times being compared by measuring the phase difference
    • G01S1/304Analogous systems in which a beat frequency, obtained by heterodyning the signals, is compared in phase with a reference signal obtained by heterodyning the signals in a fixed reference point and transmitted therefrom, e.g. LORAC (long range accuracy) or TORAN systems

Landscapes

  • Engineering & Computer Science (AREA)
  • Power Engineering (AREA)
  • Computer Networks & Wireless Communication (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Fittings On The Vehicle Exterior For Carrying Loads, And Devices For Holding Or Mounting Articles (AREA)
  • Position Fixing By Use Of Radio Waves (AREA)

Abstract

1278275 Radio navigation SOC D'ETUDES & D'APPLICATION DES TECHNIQUES NOUVELLES NEO-TEC 4 July 1969 [5 July 1968] 33922/69 Heading H4D Relates to a radio hyperbolic position-finding method, and corresponding receiving apparatus, in which families of hyperbole are defined by audio-frequency beats of different sensitivities the " partial " (i.e. within 2 II) phases E i of which are given by K i + K i X where K i represents phase at a known location, K i is the sensitivity (i.e. related to the characteristic frequency e.g. 300 kHz and a beat frequency of f 0 80 Hz), and x represents the hyperbola on which the receiver is located. According to the invention local signals of phases k i + K i x<SP>1</SP> are generated, where x<SP>1</SP> represents an estimate of x, difference signals # i representing the differences between phases k i <SP>1</SP> + K i x<SP>1</SP> and k i + K i x are produced and linear combinations of difference signals are utilized to control x<SP>1</SP> so that it tends to x. The purpose of the invention is to remove ambiguity in position determination. Transmitting systems of the embodiments are of the types named " single-signal " or " twosignal " with reference signal and in both types spaced stations B, C radiate on frequencies F, F + f 0 respectively, and a third station A radiates a carrier of frequency F 0 modulated at frequency f 0 . In the " single-signal " type, a known point D receives all the transmissions and controls the frequency at station B (or C) such that the beat frequency f 0 at D is in phase with the demodulated f 0 at D; in the " twosignal " type the point D compares the transmissions from B and C to give the frequency f 0 which is then sent to A for modulation on to F 0 . Thus in the "single-signal" type the audio frequency (AF) signals produced at a receiver are stable in frequency and phase and are processed successively whereas in the "two-signal" type the A.F. Signals are processed in pairs. Transmissions from the stations may be simultaneous or sequential and the reference signal may be omitted, a second pair of stations B, C being utilized. " Single-signal " receiver, with reference signal, Fig. 3.-In the case considered there are produced successively at the receiver a reference- A.F. of phase #-=k 0 , a first position-A.F. of phase # 1 = k 1 + K 1 x (characteristic frequency (C.F.) corresponding to K 1 of 300 kHz) and a second position-A.F. of phase # 2 = k 2 + K 2 x (C.F. 310 kHz). Assuming that x is fixed, a memory 4 stores a quantity k 0 <SP>1</SP> representing a phase # 0 , a detector 3 compares the phase 90 with # 0 and controls memory 4 until k 0 <SP>1</SP> = k 0 ; and similarly for # 1 = k 1 <SP>1</SP> + K 1 x<SP>1</SP> to correct k 1 <SP>1</SP> in memory 5 such that k 1 + K 1 x = k 1 <SP>1</SP> + K 1 x<SP>1</SP> and for memory 6 such that k 2 + K 2 x = k 2 <SP>1</SP> + K 2 x<SP>1</SP>. If there are defined quantities: further quantities, e.g. are formed since a # 2 may be > 2#, and # 1 controls x<SP>1</SP> such that # 1 #O 1 and the " sensitivity " of the correction corresponds to 10 kHz, the resulting magnitude of x being not highly accurate but substantially unambiguous. To improve accuracy another quantity #, e.g. # 2 = # 1 - # 0 (of sensitivity # 300 kHz) may be utilized. Other signals, e.g. corresponding to a C.F. of 50 kHz may be processed. It is stated that similar considerations may be applied without reference signal transmission. If the receiver is moving a velocity memory 12 is added and varies the content x<SP>1</SP> of store À7; magnitude # 2 provides correction. Detector 3 comprises a phase comparator 14, Fig. 4, producing a rectangular waveform 15, Fig. 4a, of mark/space ratio dependent on phase difference of signals on lines 2, 9, the mark/space ratio being 1 : 1 when the phase difference is zero. The waveform is applied directly to a gate 21 and after inversion 24, Fig. 4a, to a gate 18, both gates being fed with clock pulses and such that outputs 26, 27, Fig. 4a, ensue. Integrating counter-dividers 19, 22 (which are reset after each signal processing) are provided and converters 20, 23 produce pulses which define the phase in magnitude and sign and are sent to an appropriate processing circuit via a selector 28. Such a processing circuit 5 comprises a " +/- " unit 29, fed additionally with clock pulses, and a counter-divider 30 together forming the memory 5 (see also Fig. 3) for k<SP>1</SP> 1 . Pulses applied to the " + " input of unit 29 add to clock pulses and vice-versa. Phase comaprator 14 comprises gates forming a NOT-EXCLUSIVE-OR logic circuit, Figs. 6, 6a (neither shown) including a preferred variant to ensure that the output waveform mark/space ratio is 1 : 1 when the inputs are in phase, Fig. 6b (not shown). The local signals from unit 8, Fig. 3, are produced from x<SP>1</SP> and k i <SP>1</SP> magnitudes by a counter arrange. ment, Fig. 5 (not shown). Further details include: (i) when the phase difference is not small (e.g. on initial operation) the above arrangement, Fig. 4, may be too slow and an alternative arrangement producing waveforms for the " +/- " unit 29 of Fig. 4 such that when the input signals are in phase two zero-level outputs ensue for application to the " +1- " unit, Figs. 7a ... 7d (none shown); (ii) a circuit for producing signals representing the difference # 1 = k 2 <SP>1</SP> - k 1 <SP>1</SP> (it being contrived that k 1 = k 2 ) incorporates " JK " bistables, Figs. 8a ... 8d (none shown) or Figs. 9a, 9b (neither shown), the latter not requiring symmetrical input signals; (iii) a " +/- " circuit incorporating " JK " bi-stables and an adder, Fig. 11 or Fig. 13 (neither shown); and (iv) a variant of the Fig. 3 embodiment, Fig. 14 (not shown). " Two-signal " receiver, Fig. 16.-In the " two-signal " case each of a pair of A.F. signals from receiver 90 are produced simultaneously on lines 91, 92 respectively and applied to phase comparators 101, 102 of the kind corresponding to Fig. 6 (see above) and their outputs are applied to a unit 103, e.g. as described above with reference to Fig. 4. The circuit of Fig. 14 (see above) is varied to yield simultaneous processing Fig. 15 (not shown). Three pairs of A.F. signals are utilized, each pair comprising a reference and a position-finding signal.
GB33922/69A 1968-07-05 1969-07-04 Radio hyperbolic navigation Expired GB1278275A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR158011 1968-07-05

Publications (1)

Publication Number Publication Date
GB1278275A true GB1278275A (en) 1972-06-21

Family

ID=8652135

Family Applications (1)

Application Number Title Priority Date Filing Date
GB33922/69A Expired GB1278275A (en) 1968-07-05 1969-07-04 Radio hyperbolic navigation

Country Status (3)

Country Link
US (1) US3689926A (en)
FR (1) FR1586676A (en)
GB (1) GB1278275A (en)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3754260A (en) * 1971-12-02 1973-08-21 Beukers Labor Inc Loran-c third cycle identification through the use of omega
FR2500171A1 (en) * 1981-02-13 1982-08-20 Mlr Electronique METHOD OF RADIO-LOCALIZATION BY DETERMINATION OF ELECTROMAGNETIC WAVE PHASES AND RECEIVER DISPSOSITIVE FOR IMPLEMENTING SAID METHOD
FR2500168A1 (en) * 1981-02-16 1982-08-20 Juzhnoe Proizv Obiedin Digital sequential phase meter - measures phase differences using simplified control pulse divider maintaining linear dynamic characteristic
US4492963A (en) * 1983-10-05 1985-01-08 Eg&G, Inc. Method and apparatus for determining lane count error in a radio navigational system
EP0159844A3 (en) * 1984-04-19 1986-08-20 Cubic Western Data Multi-frequency lane identification system
US6968737B2 (en) * 1997-01-02 2005-11-29 Lucent Technologies Inc. Position determining system using transmitted position information

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3214759A (en) * 1962-04-19 1965-10-26 Seismograph Service Corp Apparatus for providing lane identifi, cation in hyperbolic position finding systems

Also Published As

Publication number Publication date
US3689926A (en) 1972-09-05
FR1586676A (en) 1970-02-27

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Legal Events

Date Code Title Description
PS Patent sealed [section 19, patents act 1949]
PCNP Patent ceased through non-payment of renewal fee