GB1319634A - Navigation systems - Google Patents

Navigation systems

Info

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
Application number
GB3722270A
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.)
Teledyne Inc
Original Assignee
Teledyne Inc
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 Teledyne Inc filed Critical Teledyne Inc
Publication of GB1319634A publication Critical patent/GB1319634A/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
    • G01S1/20Systems 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
    • G01S1/308Systems 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.
GB3722270A 1969-08-01 1970-07-31 Navigation systems Expired GB1319634A (en)

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)

* Cited by examiner, † Cited by third party
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

Also Published As

Publication number Publication date
DE2035202B2 (en) 1978-12-07
DE2035202A1 (en) 1971-02-11
DE2035202C3 (en) 1979-08-02

Similar Documents

Publication Publication Date Title
GB940508A (en) Doppler radio navigation system
US3852750A (en) Navigation satellite system
GB946978A (en) Improvements in or relating to radar systems
GB1480490A (en) Transmission of radio navigation phase corrections
US3230453A (en) System for maintaining fixed phase between a pair of remotely located stations
GB1349861A (en) Antenna direction control system
GB1104861A (en) Improvements in or relating to aircraft radio landing aids
US3339202A (en) Radiolocation system transmitting sideband signals
GB1319634A (en) Navigation systems
GB1121353A (en) Communication system
US3648177A (en) Transmitter for distance-measuring system
GB1368829A (en) Radar systems
GB1371952A (en) Method of and apparatus for providing phase corrections in particular for the omega radio-navigation system
US2976363A (en) Modulation of selected phases of carriers for simultaneous transmission through single delay means
US3325811A (en) Radio navigation system
GB1087188A (en) Communication system
GB1065818A (en) Radio location ranging system
GB1096452A (en) Electric signal transmission system
GB1003317A (en) Radio navigational system
GB1278275A (en) Radio hyperbolic navigation
GB1161798A (en) Method and Means for Radiolocation of a Radio Receiving Station
US3346860A (en) Radio navigation system
GB1145783A (en) Radar system for measuring position and velocity of a distant object
GB1146429A (en) Phase difference measuring system
GB1086924A (en) Tracking system for a communication satellite

Legal Events

Date Code Title Description
PS Patent sealed
PCNP Patent ceased through non-payment of renewal fee