GB1289741A - - Google Patents
Info
- Publication number
- GB1289741A GB1289741A GB1289741DA GB1289741A GB 1289741 A GB1289741 A GB 1289741A GB 1289741D A GB1289741D A GB 1289741DA GB 1289741 A GB1289741 A GB 1289741A
- Authority
- GB
- United Kingdom
- Prior art keywords
- phase shift
- plane
- targets
- aerials
- azimuth
- 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
- G01S13/00—Systems using the reflection or reradiation of radio waves, e.g. radar systems; Analogous systems using reflection or reradiation of waves whose nature or wavelength is irrelevant or unspecified
- G01S13/66—Radar-tracking systems; Analogous systems
- G01S13/68—Radar-tracking systems; Analogous systems for angle tracking only
- G01S13/685—Radar-tracking systems; Analogous systems for angle tracking only using simultaneous lobing techniques
-
- 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
- G01S13/00—Systems using the reflection or reradiation of radio waves, e.g. radar systems; Analogous systems using reflection or reradiation of waves whose nature or wavelength is irrelevant or unspecified
- G01S13/02—Systems using reflection of radio waves, e.g. primary radar systems; Analogous systems
- G01S13/06—Systems determining position data of a target
- G01S13/42—Simultaneous measurement of distance and other co-ordinates
- G01S13/44—Monopulse radar, i.e. simultaneous lobing
- G01S13/4454—Monopulse radar, i.e. simultaneous lobing phase comparisons monopulse, i.e. comparing the echo signals received by an interferometric antenna arrangement
Landscapes
- Engineering & Computer Science (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Computer Networks & Wireless Communication (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Variable-Direction Aerials And Aerial Arrays (AREA)
- Radar Systems Or Details Thereof (AREA)
Abstract
1289741 Monopulse radar LICENTIA PATENT VERWALTUNGS GmbH 24 Dec 1969 [9 Jan 1969] 62915/69 Heading H4D In a phase monopulse radar, angular deviation, in two planes, e.g. azimuth and elevation, of targets from the aerial boresight is measured using five aerials, three for each plane, and for each plane combining the signals received at each aerial V 1 , V 2 , V 3 to produce the quantities (V 1 eiu1 - V 2 ), (V 2 eiu<SP>1</SP> - V 3 ) and (V 1 eiu 1 - V 2 )eiu<SP>2</SP>, where u 1 and u 2 are proportional to the azimuth or elevation angular displacements of two targets, the above quantities being used to determine u 1 and u 2 . In a first embodiment, five aerials are used in a cruciform in a plane Lr to the aerial boresight, Fig. 3. The signals received by the three aerials in the azimuth plane are given by where An = signal amplitude from target n U n = K.l.sinα n K =2#/# i α n = azimuth angle of target n l = displacement of adjacent aerials. These signals are fed to apparatus, Fig. 5, wherein V 1 undergoes a phase shift, V 2 is subtrated therefrom and the amplitude of the resultant is detected and compared with a signal derived from V 2 and V 3 in a similar manner. The above equations show that if this difference in amplitude is zero, the phase shift of V 1 and V 2 is u 1 = K.l.sinα 1 . Thus the difference signal is utilized in a feedback loop to control the two phase shift elements and the final value of phase shift determines α 1 . The equations also show that Thus the signals produced above are subtracted after the former has undergone a phase shift and the difference is fed-back to control the phase shift element. At balance the value of phase shift is u 2 =Klsinα 2 . The same procedure us used to derive the two elevation angles # 1 , # 2 . This method however gives two possible sets of co-ordinates, shown in Fig. 6 as circles and crosses respectively. In order to correlate the co-ordinates to each other, the aerial is swivelled until the boresight bisects the two azimuth angles and the two elevation angles. It is then rotated anti-clockwise about the boresight. If the elevation angles become zero first, the circles denote the targets: if the azimuth angles become zero first, the crosses denote the targets. If only one target is present, the first phase shift control voltage is zero for whatever phase shift is applied and the co-ordinates of the single target are obtained from the second phase shift elements in each plane. The same general principles are described as being applied to a system for resolving three targets (Fig. 8, not shown). In this case seven aerials are used, one extra for each plane. The correlation procedure also applies the same procedure but is much more complex. In general, to resolve v targets v + 1 aerials are used in each plane with one aerial common to both planes.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE19691900854 DE1900854A1 (en) | 1969-01-09 | 1969-01-09 | Procedure for radar multiple target detection |
Publications (1)
Publication Number | Publication Date |
---|---|
GB1289741A true GB1289741A (en) | 1972-09-20 |
Family
ID=5721972
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1289741D Expired GB1289741A (en) | 1969-01-09 | 1969-12-24 |
Country Status (2)
Country | Link |
---|---|
DE (1) | DE1900854A1 (en) |
GB (1) | GB1289741A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2417118A1 (en) * | 1978-02-09 | 1979-09-07 | Siemens Ag Albis | ANGULAR MEASUREMENT METHOD IN A TRACKING RADAR |
GB2429860A (en) * | 2005-08-31 | 2007-03-07 | Roke Manor Research | Phased array radar |
CN110986947A (en) * | 2019-11-29 | 2020-04-10 | 重庆交通大学 | Multi-target self-propelled ship model track tracking measurement method |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
LU87671A1 (en) * | 1990-01-31 | 1990-05-15 | Ceodeux Sa | TAP FOR COMPRESSED OR LIQUIFIED GAS |
FR2666904B1 (en) * | 1990-09-18 | 1993-02-12 | Snecma | CONTINUOUS TRANSMISSION RADAR DEVICE FOR THE SHORT-TERM DETERMINATION OF THE RELATIVE POSITION BETWEEN A MISSILE AND A TARGET MACHINE ON WHICH IT IS MOUNTED. |
-
1969
- 1969-01-09 DE DE19691900854 patent/DE1900854A1/en active Pending
- 1969-12-24 GB GB1289741D patent/GB1289741A/en not_active Expired
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2417118A1 (en) * | 1978-02-09 | 1979-09-07 | Siemens Ag Albis | ANGULAR MEASUREMENT METHOD IN A TRACKING RADAR |
GB2429860A (en) * | 2005-08-31 | 2007-03-07 | Roke Manor Research | Phased array radar |
GB2429860B (en) * | 2005-08-31 | 2007-08-15 | Roke Manor Research | Phased array radar |
CN110986947A (en) * | 2019-11-29 | 2020-04-10 | 重庆交通大学 | Multi-target self-propelled ship model track tracking measurement method |
CN110986947B (en) * | 2019-11-29 | 2023-05-02 | 重庆交通大学 | Multi-target self-navigation ship model track tracking measurement method |
Also Published As
Publication number | Publication date |
---|---|
DE1900854A1 (en) | 1970-08-13 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PS | Patent sealed | ||
PCNP | Patent ceased through non-payment of renewal fee |