GB1319634A - Navigation systems - Google Patents
Navigation systemsInfo
- Publication number
- GB1319634A GB1319634A GB3722270A GB3722270A GB1319634A GB 1319634 A GB1319634 A GB 1319634A GB 3722270 A GB3722270 A GB 3722270A GB 3722270 A GB3722270 A GB 3722270A GB 1319634 A GB1319634 A GB 1319634A
- Authority
- GB
- United Kingdom
- Prior art keywords
- phase
- received
- signals
- station
- comparators
- 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
-
- 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
- G01S1/20—Systems 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
- G01S1/30—Systems 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
- G01S1/308—Systems 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 particularly adapted to Omega systems
Landscapes
- Engineering & Computer Science (AREA)
- Computer Networks & Wireless Communication (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Position Fixing By Use Of Radio Waves (AREA)
- Radio Relay Systems (AREA)
Abstract
1319634 Radio navigation TELEDYNE Inc 31 July 1970 [1 Aug 1969] 37222/70 Heading H4D In an OMEGA phase comparison navigation system adapted to overcome skywave interference, a relay station 16, Fig. 1 is provided at a fixed known position in the vicinity of the mobile station 18, such that it may be assumed that the signals received at the relay station from the transmitting stations A, B, and C undergo the same skywave phase shifts # A , # B # C as do those received by the mobile station. The use of the 10À2 KH 3 transmission only is described. At the relay station (Fig. 3, not shown) each received 10À2 KH 3 signals mixed with the output of a phase locked oscillator at 10À5 KH 3 , to give a 300 H 3 signal phase locked to the received 10À2 KH 3 signal, which 300 H 3 signal is amplitude modulated on to a 1750 KH 3 carrier. At the mobile station the 10À2 KH 3 signal from station A is received at receiver 24 with a phase shift # A18 + # A and the modulated relay carrier is received at 22 with a phase shift #A.16+#A+# 16À18 , where # AÀ18 , # A16 and # 16À18 are the propagation phase shifts between stations A and the mobile stations 18, between stations A and the relay station and between the relay station and the mobile station, respectively. The receivers 22 and 24 produce signals of equal frequency from the received signals, phase locked therewith, and feed these via synchronous commutators 26, 28 operating in synchronism with the transmission - to a phase comparator 30. The phase difference presented at 30 and indicated thereby is: # A.16 - # A18 +# 16.18 , i.e. the skywave effect is cancelled out. Similarly phase comparators 32 and 34, respectively receiving the direct and relayed transmission from stations B and C indicate: # B.16 - # B.18 +# 16.18 and The comparators have shaft rotation outputs such that mechanised differentials 36 and 38 coupled to the shafts of comparators 30/32 and 32/34 respectively, give outputs at 40 and 42 indicative of the phase differences: Since the relay has a known position the terms (# A16 - # B.16 ) and (# B.16 - # C16 ) one known and can be compensated for, thereby leaving the position line defining phase differences, In the arrangement of Fig. 2 (not shown), the differential resolves 44 and 46 are used as phase shifters to shift the phases of the A station signals received by receiver 24 and receiver 22 respectively under the control of phase comparator 32. Comparators 40 and 42 then determine the phase differences between the respective phase shifted signals and the signals from receivers 22 and 24 to give the same indicated final indications on 40 and 42 as given above. The phase comparators 30, 32, &c. may be replaced by balanced mixers feeding phase storage means (Fig. 5, not shown). The phase storage means may be updated by navigational aids e.g. inertial nagivation means and may comprise (Fig. 6, not shown) a phase detector detecting the phase difference between the balanced mixer output and that of a voltage controlled oscillator. The intermittent detector output is stored in an integrator, being fed as a continuous signal to control the oscillator. The output of the oscillator constitutes the output of the phase storage means.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US84753769A | 1969-08-01 | 1969-08-01 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB1319634A true GB1319634A (en) | 1973-06-06 |
Family
ID=25300879
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB3722270A Expired GB1319634A (en) | 1969-08-01 | 1970-07-31 | Navigation systems |
Country Status (2)
Country | Link |
---|---|
DE (1) | DE2035202C3 (en) |
GB (1) | GB1319634A (en) |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4870422A (en) * | 1982-03-01 | 1989-09-26 | Western Atlas International, Inc. | Method and system for determining position from signals from satellites |
US5619212A (en) | 1982-03-01 | 1997-04-08 | Western Atlas International, Inc. | System for determining position from suppressed carrier radio waves |
DE3909758A1 (en) * | 1989-03-23 | 1990-10-04 | Fraunhofer Ges Forschung | Method for self-location of moving objects on the basis of long-wave, mutually phase-locked signals |
-
1970
- 1970-07-16 DE DE19702035202 patent/DE2035202C3/en not_active Expired
- 1970-07-31 GB GB3722270A patent/GB1319634A/en not_active Expired
Also Published As
Publication number | Publication date |
---|---|
DE2035202B2 (en) | 1978-12-07 |
DE2035202A1 (en) | 1971-02-11 |
DE2035202C3 (en) | 1979-08-02 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PS | Patent sealed | ||
PCNP | Patent ceased through non-payment of renewal fee |