GB1003317A - Radio navigational system - Google Patents
Radio navigational systemInfo
- Publication number
- GB1003317A GB1003317A GB2751061A GB2751061A GB1003317A GB 1003317 A GB1003317 A GB 1003317A GB 2751061 A GB2751061 A GB 2751061A GB 2751061 A GB2751061 A GB 2751061A GB 1003317 A GB1003317 A GB 1003317A
- Authority
- GB
- United Kingdom
- Prior art keywords
- signal
- phase
- harmonic
- aerial
- bearing
- 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
Links
Classifications
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q1/00—Details of, or arrangements associated with, antennas
- H01Q1/52—Means for reducing coupling between antennas; Means for reducing coupling between an antenna and another structure
- H01Q1/521—Means for reducing coupling between antennas; Means for reducing coupling between an antenna and another structure reducing the coupling between adjacent antennas
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01S—RADIO 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
- G01S1/00—Beacons 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
- G01S1/02—Beacons 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
- G01S1/08—Systems for determining direction or position line
- G01S1/38—Systems for determining direction or position line using comparison of [1] the phase of the envelope of the change of frequency, due to Doppler effect, of the signal transmitted by an antenna moving, or appearing to move, in a cyclic path with [2] the phase of a reference signal, the frequency of this reference signal being synchronised with that of the cyclic movement, or apparent cyclic movement, of the antenna
- G01S1/40—Systems for determining direction or position line using comparison of [1] the phase of the envelope of the change of frequency, due to Doppler effect, of the signal transmitted by an antenna moving, or appearing to move, in a cyclic path with [2] the phase of a reference signal, the frequency of this reference signal being synchronised with that of the cyclic movement, or apparent cyclic movement, of the antenna the apparent movement of the antenna being produced by cyclic sequential energisation of fixed antennas
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)
- Variable-Direction Aerials And Aerial Arrays (AREA)
Abstract
1,003,317. Omni range navigation systems. STANDARD TELEPHONES & CABLES Ltd. July 27, 1962 [July 28, 1961], No. 27510/61. Heading H4D. In a commuted aerial or rotating aerial Doppler type V.O.R. system wherein the reference carrier wave is modulated with a first signal and the bearing signal derived from the phase - modulated signal received from the commuted aerials is compared at the receiver with the said first signal, the reference carrier wave is further modulated with a harmonic of the first signal, and a harmonic of the bearing signal derived by means of a phase discriminator is compared at the receiver with the said harmonic of the first signal. Such an arrangement provides an ambiguous fine bearing value from the said harmonic comparison in addition to the normal unambiguous course bearing value. In the arrangement of Fig. 4 an R/F signal from generator 37 is shifted through 9960 c/s. by an oscillator 41 and a single side-band modulator 40, and the resulting signal is fed via wire 42 to a capacitive rotor plate 44, which is rotated at 30 c/s. by a motor 35 and which feeds the signal to the 36 aerial in succession. The R/F signal from generator 37 is also amplitude modulated in modulator 38 with a 30 c/s. signal from a generator 36 coupled in synchronism with the motor 35 and is fed, as a reference signal, to the central fixed aerial 32. Harmonics of the signal from generator 36 are produced by harmonic generator 46 and the 9th or 270 c/s. harmonic is selected by filter 47 and fed to the modulator 38 to further amplitude modulate the reference signal. The arrangement of Fig. 5 is similar except that the balanced earthed loads 66 are substituted for alternate aerials and the aerials are fed with upper and lower side-bands (F+9960) c/s. and (F - 9960) c/s. through plates 64 and 67 respectively, the two plates being diametrically opposite and only one plate coupling to an aerial at a time. This arrangement results in a larger Doppler shift than in the arrangement of Fig. 4. A receiver, Figs. 2, 3, compatible with standard V.O.R. systems, comprises a second A.M. detector 10 feeding a L/F output circuit 11, the output of which comprises a 30 c/s. reference signal, a 270 c/s. reference signal, and a phasemodulated 9960 c/s. bearing signal, the maximum frequency deviation being Œ 480 c/s. at zero elevation at a repetition rate of 30 c/s. This 30 c/s. phase modulation repetition rate signal is detected in F.M. discriminator 17 and compared in phase with the 30 c/s. reference signal from filter 13, to give a rough unambiguous bearing value. The 9960 c/s. signal is also fed to a phase discriminator 14 which yields, together with filter 15, a 270 c/s. phase-locked signal for comparison with the 270 c/s. reference signal from filter 16, to give a fine ambiguous bearing value. Alternatively the outputs of discriminators 14 and 17 may be combined to give bearing information as described in Specification 694,549. The phase discriminator 14 is a harmonic phase discriminator working on principles given in Specification 695,085. It essentially comprises a phase discriminator 26 having the phase modulated 9960 c/s. signal at one input 27 and the said signal delayed in 25 to be in phase quadrature, at the other input 28. Such an arrangement gives a 270 c/s. output signal at 29. Harmonics other than the 9th may be less advantageously used, the omission of the delay network 25 giving even harmonics. The invention is said to be applicable to true Doppler systems comprising a bodily rotating aerial. The 270 c/s. reference signal may be transmitted on a separate carrier or on a sideband of the first carrier. Specification 899,951 also is referred to.
Priority Applications (6)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB2751061A GB1003317A (en) | 1961-07-28 | 1961-07-28 | Radio navigational system |
CH879262A CH410072A (en) | 1961-07-28 | 1962-07-23 | Omni-directional radio navigation system |
FR905116A FR1329895A (en) | 1961-07-28 | 1962-07-26 | Radio navigation system |
DEJ22165A DE1190525B (en) | 1961-07-28 | 1962-07-28 | Doppler radio beacon system with fine azimuth display on the receiver side |
GB4061962A GB1013917A (en) | 1961-07-28 | 1962-10-26 | Radio aerial arrangement |
FR951777A FR84586E (en) | 1961-07-28 | 1963-10-25 | Radio navigation system |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB2751061A GB1003317A (en) | 1961-07-28 | 1961-07-28 | Radio navigational system |
Publications (1)
Publication Number | Publication Date |
---|---|
GB1003317A true GB1003317A (en) | 1965-09-02 |
Family
ID=10260743
Family Applications (2)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB2751061A Expired GB1003317A (en) | 1961-07-28 | 1961-07-28 | Radio navigational system |
GB4061962A Expired GB1013917A (en) | 1961-07-28 | 1962-10-26 | Radio aerial arrangement |
Family Applications After (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB4061962A Expired GB1013917A (en) | 1961-07-28 | 1962-10-26 | Radio aerial arrangement |
Country Status (3)
Country | Link |
---|---|
CH (1) | CH410072A (en) |
DE (1) | DE1190525B (en) |
GB (2) | GB1003317A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3448453A (en) * | 1966-07-08 | 1969-06-03 | Int Standard Corp | Doppler vor systems |
US3787861A (en) * | 1970-12-11 | 1974-01-22 | Thomson Csf | Improvements in doppler instrument landing systems |
EP1329737A2 (en) * | 2002-01-18 | 2003-07-23 | Hewlett-Packard Company | Location system using beacon transmitters |
Families Citing this family (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE3027451A1 (en) * | 1980-07-19 | 1982-02-11 | Standard Elektrik Lorenz Ag, 7000 Stuttgart | ANTENNA ARRANGEMENT WITH SEVERAL ANTENNAS |
US5369413A (en) * | 1993-07-02 | 1994-11-29 | Hazeltine Corp. | Q equalization in dual-element end-fire array antennas |
CN111478044B (en) * | 2020-03-31 | 2022-03-29 | Oppo广东移动通信有限公司 | Antenna module and terminal |
DE102020110348B3 (en) * | 2020-04-15 | 2021-08-05 | Bundesrepublik Deutschland, Vertreten Durch Das Bundesministerium Für Wirtschaft Und Energie, Dieses Vertreten Durch Den Präsidenten Der Physikalisch-Technischen Bundesanstalt | Method for transmitting data between a base station and a mobile station and data transmission system |
-
1961
- 1961-07-28 GB GB2751061A patent/GB1003317A/en not_active Expired
-
1962
- 1962-07-23 CH CH879262A patent/CH410072A/en unknown
- 1962-07-28 DE DEJ22165A patent/DE1190525B/en active Pending
- 1962-10-26 GB GB4061962A patent/GB1013917A/en not_active Expired
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3448453A (en) * | 1966-07-08 | 1969-06-03 | Int Standard Corp | Doppler vor systems |
US3787861A (en) * | 1970-12-11 | 1974-01-22 | Thomson Csf | Improvements in doppler instrument landing systems |
EP1329737A2 (en) * | 2002-01-18 | 2003-07-23 | Hewlett-Packard Company | Location system using beacon transmitters |
EP1329737A3 (en) * | 2002-01-18 | 2004-07-28 | Hewlett-Packard Company | Location system using beacon transmitters |
Also Published As
Publication number | Publication date |
---|---|
GB1013917A (en) | 1965-12-22 |
CH410072A (en) | 1966-03-31 |
DE1190525B (en) | 1965-04-08 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US3752992A (en) | Optical communication system | |
US2253958A (en) | Rotating radio beacon | |
US3290677A (en) | Continuous wave angle and range determining radar | |
GB899951A (en) | Radio navigation system | |
GB811762A (en) | Improvements in devices for determining position by means of the transit time of radiated waves | |
US6057798A (en) | Apparatus and method for frequency modulation | |
US3789398A (en) | Fm-cw radar range system | |
GB1003317A (en) | Radio navigational system | |
US3197773A (en) | Frequency modulated continuous wave navigation radar | |
US3320364A (en) | System for phase coding information by blanking half cycles of a continuous periodicwave | |
US3628155A (en) | Amplitude modulation intensifier method and apparatus | |
US3340533A (en) | Radio direction finding system | |
GB1017108A (en) | Improvements in or relating to radio navigation systems utilizing satellites | |
GB1349861A (en) | Antenna direction control system | |
US4183022A (en) | Transponder for radiocommunication system, particularly for measuring the distance between two stations | |
US2543448A (en) | Moving object radio pulse-echo system | |
US3648177A (en) | Transmitter for distance-measuring system | |
GB758139A (en) | Radio direction finding system | |
US2976363A (en) | Modulation of selected phases of carriers for simultaneous transmission through single delay means | |
GB1048328A (en) | Radio communication system | |
US2457137A (en) | Ultra high frequency system | |
US2551828A (en) | Radio beacon | |
US3766482A (en) | Radiant energy receivers | |
US3502989A (en) | Receiver employing correlation techniques | |
GB1024242A (en) | Radio navigation system |