GB1428682A - Elevation-measuring system - Google Patents
Elevation-measuring systemInfo
- Publication number
- GB1428682A GB1428682A GB2732673A GB2732673A GB1428682A GB 1428682 A GB1428682 A GB 1428682A GB 2732673 A GB2732673 A GB 2732673A GB 2732673 A GB2732673 A GB 2732673A GB 1428682 A GB1428682 A GB 1428682A
- Authority
- GB
- United Kingdom
- Prior art keywords
- pulses
- group
- phase
- pulse
- amplitude
- 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
- G01S1/44—Rotating or oscillating beam beacons defining directions in the plane of rotation or oscillation
-
- 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
- G01S1/302—Systems in which the direction is determined by using an interferometric type transmitting antenna array
Landscapes
- Engineering & Computer Science (AREA)
- Remote Sensing (AREA)
- Computer Networks & Wireless Communication (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Radar, Positioning & Navigation (AREA)
- Radar Systems Or Details Thereof (AREA)
- Variable-Direction Aerials And Aerial Arrays (AREA)
Abstract
1428682 Radio-navigation; aerials INTERNATIONAL STANDARD ELECTRIC CORP 8 June 1973 [22 June 1972] 27326/73 Headings H4A and H4D In an elevation measuring system a ground station has a vertical linear aerial array of n equally spaced radiators which are cyclically and sequentially excited with pulses of R.F. energy having equal magnitudes and the same phases, a characteristic pulse train being radiated before each cycle of pulses. At an airborne receiving station the phase and amplitude of each pulse in a cycle are measured relatively to one of them, for example, to the first pulse, and at least two different groups are formed, each containing m successive received pulses (where m is less than n). The phase and amplitude of each pulse in each group are changed, the changes for corresponding pulses of all groups being the same, and the vector sum of the changed pulses of each group is determined. The elevation is determined from the phase differences of the said vector sums. As described, the ground station aerial array comprises 40 parallel dipoles, at half-wavelength spacings. In a cycle, the characterizing pulse train is first sent from radiator no. 1. The radiators are then connected in order, from no. 1 to no. 40, to the transmitter and radiate pulses of R.F. waves, whose amplitudes and phases are equal for all radiators. At the airborne station the characterizing pulse train, after conversion to I.F., is recognized by a device 15, Fig. 3, which alerts a computer 13 and sets a switch 8 to its upper contact (as shown). The first received pulse (from radiator no. 1) is applied at I.F. to an oscillator 10, which is thereby synchronized with respect to amplitude and phase. After the first pulse, the switch 8 is changed to its lower contact, and the succeeding pulses are applied through an I.F. amplifier 9 to an amplitude meter 11 and a phase meter 12. The phase and the amplitude of the output signal of the oscillator 10, which is coupled to second inputs of the meters 11, 12, serve as reference quantities for the measurements made in respect of the second to fortieth pulses. The outputs of the meters 11, 12 are connected to the computer 13, output from which operates an indicator 14. The stored values of phases and amplitudes are processed by the computer in groups of twenty successive pulses each, i.e., those corresponding to respective radiators nos. 1 to 20 (group O), nos. 21 to 40 (group F), nos. 2 to 21 (group G), and nos 5 to 24 (group Z). The changes effected to the pulses in each group may be such as to produce a virtual radiation pattern for use at high elevations in which the field strength is approximately equal at all angles, or to produce a peaked virtual radiation pattern for use at low elevations (Figs. 1, 2, not shown). In determining the elevation, use of the two groups O and F provides maximum accuracy, but the result is ambiguous, since their equivalent phase centres on the transmitting array are ten wavelengths apart. Use is therefore made of the groups G and Z, each taken with the group O, to resolve the ambiguity, since their equivalent phase centres are respectively only a half-wavelength and two wavelengths from that of the group O. Specification 1,410,121 is mentioned.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE19722230630 DE2230630C (en) | 1972-06-22 | Radio navigation system for elevation measurement using the phase difference method |
Publications (1)
Publication Number | Publication Date |
---|---|
GB1428682A true GB1428682A (en) | 1976-03-17 |
Family
ID=5848514
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB2732673A Expired GB1428682A (en) | 1972-06-22 | 1973-06-08 | Elevation-measuring system |
Country Status (7)
Country | Link |
---|---|
JP (1) | JPS5234358B2 (en) |
CA (1) | CA1001742A (en) |
DE (1) | DE2230630B1 (en) |
ES (1) | ES416187A1 (en) |
FR (1) | FR2189747B3 (en) |
GB (1) | GB1428682A (en) |
IT (1) | IT989186B (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2396501A (en) * | 2000-02-23 | 2004-06-23 | Fujitsu Ltd | Directing radio beam |
US6864839B2 (en) | 2000-02-23 | 2005-03-08 | Fujitsu Limited | Radio transceiver and method of controlling direction of radio-wave emission |
Families Citing this family (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS50148177U (en) * | 1974-05-24 | 1975-12-09 | ||
DE2717997C2 (en) * | 1977-04-22 | 1982-04-29 | Standard Elektrik Lorenz Ag, 7000 Stuttgart | Monopulse direction finder for azimuth and / or elevation measurement |
JPS56118521U (en) * | 1980-02-08 | 1981-09-10 | ||
JPS60177321U (en) * | 1984-05-07 | 1985-11-25 | 三菱自動車工業株式会社 | nut plate |
-
1972
- 1972-06-22 DE DE19722230630D patent/DE2230630B1/en active Granted
-
1973
- 1973-06-08 GB GB2732673A patent/GB1428682A/en not_active Expired
- 1973-06-15 IT IT2539173A patent/IT989186B/en active
- 1973-06-21 CA CA174,657A patent/CA1001742A/en not_active Expired
- 1973-06-22 ES ES416187A patent/ES416187A1/en not_active Expired
- 1973-06-22 JP JP6992873A patent/JPS5234358B2/ja not_active Expired
- 1973-06-22 FR FR7322870A patent/FR2189747B3/fr not_active Expired
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2396501A (en) * | 2000-02-23 | 2004-06-23 | Fujitsu Ltd | Directing radio beam |
GB2396501B (en) * | 2000-02-23 | 2004-11-17 | Fujitsu Ltd | Radio transmitter and method of controlling direction of radio-wave emission |
US6864839B2 (en) | 2000-02-23 | 2005-03-08 | Fujitsu Limited | Radio transceiver and method of controlling direction of radio-wave emission |
US7391371B2 (en) | 2000-02-23 | 2008-06-24 | Fujitsu Limited | Radio transceiver and method of controlling direction of radio-wave emission |
Also Published As
Publication number | Publication date |
---|---|
FR2189747B3 (en) | 1976-06-18 |
ES416187A1 (en) | 1976-03-01 |
IT989186B (en) | 1975-05-20 |
DE2230630B1 (en) | 1973-11-08 |
AU5723373A (en) | 1975-01-09 |
JPS5234358B2 (en) | 1977-09-02 |
CA1001742A (en) | 1976-12-14 |
FR2189747A1 (en) | 1974-01-25 |
JPS4958796A (en) | 1974-06-07 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US2412702A (en) | Object detection and location | |
US2248215A (en) | Radio direction and distance indicating system | |
US3866229A (en) | Method and apparatus for automatically determining position-motion state of a moving object | |
US3378846A (en) | Method and apparatus for testing phased array antennas | |
US3973262A (en) | Radio direction finder with means for reducing sensitivity to multipath propogation errors | |
US2427029A (en) | Automatic tracking system | |
US2407287A (en) | Course beacon | |
US2423023A (en) | Obstacle detection by radio waves | |
US2407198A (en) | Distance and direction determination system | |
GB1410121A (en) | Radiolocation system and method | |
US2404196A (en) | Radio beacon system | |
US3864681A (en) | System and process for locating sources of radiation | |
US3484167A (en) | Formation flight control system | |
US2403622A (en) | Obstacle detecting system | |
US3918056A (en) | Radar trilateralization position locators | |
GB1428682A (en) | Elevation-measuring system | |
US3400398A (en) | Broadcast apparatus for position determining system | |
US3670332A (en) | Direction finding device | |
US3916407A (en) | Doppler navigation system with angle and radial velocity determination | |
US3290685A (en) | Omni-range doppler beacons and direction finding systems | |
US3670338A (en) | Radio navigation receiving equipment | |
US2803821A (en) | Radio navigation receiver | |
US3024441A (en) | Sector scan indicator | |
US3349400A (en) | Digital bearing measuring system | |
US2546970A (en) | Direction finder system |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PS | Patent sealed | ||
PCNP | Patent ceased through non-payment of renewal fee |