GB2030416A - Improvements in or relating to radar systems - Google Patents
Improvements in or relating to radar systems Download PDFInfo
- Publication number
- GB2030416A GB2030416A GB7928555A GB7928555A GB2030416A GB 2030416 A GB2030416 A GB 2030416A GB 7928555 A GB7928555 A GB 7928555A GB 7928555 A GB7928555 A GB 7928555A GB 2030416 A GB2030416 A GB 2030416A
- Authority
- GB
- United Kingdom
- Prior art keywords
- longer
- pulse
- radar system
- signals
- radar
- 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.)
- Granted
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
- G01S7/00—Details of systems according to groups G01S13/00, G01S15/00, G01S17/00
- G01S7/02—Details of systems according to groups G01S13/00, G01S15/00, G01S17/00 of systems according to group G01S13/00
- G01S7/28—Details of pulse systems
- G01S7/2813—Means providing a modification of the radiation pattern for cancelling noise, clutter or interfering signals, e.g. side lobe suppression, side lobe blanking, null-steering arrays
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q25/00—Antennas or antenna systems providing at least two radiating patterns
- H01Q25/007—Antennas or antenna systems providing at least two radiating patterns using two or more primary active elements in the focal region of a focusing device
Abstract
A radar system including an antenna 1, 2, 3 adapted to provide two beams one (feed 3) of which covers a higher elevation than the other (feed 2), and means 4 for producing two successive radar pulses one (F1) of which is longer than the other (F2), a switch 10, 11, 14, 17 for selecting in dependence upon range the beam required and for selecting a predetermined pulse length for use therewith so that when receiving signals from short ranges the shorter pulse F2 is used with the higher beam only (giving good resolution) and when receiving signals from longer ranges the longer pulse F1 is used with the lower beam only (giving good long range detection capability) and at intermediate ranges the shorter pulse is used with the lower beam whilst the longer pulse is used with the higher beam. <IMAGE>
Description
SPECIFICATION
Improvements in or relating to radar systems
This invention relates to radar systems.
It is desirable to provide a radar system which affords good target detection at short range for various altitudes whilst being capable of detecting targets at long range. It is well known that radar coverage is dependent upon antenna design and some known systems provide two antenna arrangements which in combination afford good target detection at various ranges and altitudes. It is also known that radar performance is dependent upon radar pulse length and that at long ranges a longer pulse having more energy is desirable.
However with presently proposed systems, in order to provide for optimum target detection at different ranges and altitudes, a number of radar channels are required, which involves considerable duplication of hardware and is therefore correspondingly expensive.
According to the present invention a radar system includes an antenna adapted to provide two beams one of which covers a higher elevation than the other, and means for producing two successive radar pulses one of which is longer than the other, switch means for selecting in dependence upon range the beam required and for selecting a predetermed pulse length for use therewith so that when receiving signals from short ranges the shorter pulse is used with the higher beam only and when receiving signals from longer ranges the longer pulse is used with the lower beam only and at intermediate ranges the shorter pulse is used with the lower beam whilst the longer pulse is used with the higher beam.
By using the system according to the present invention at short ranges the shorter pulse affords good resolution and the higher beam minimises signals received from ground clutter. At longer ranges a longer pulse increases the energy available to the radar and the lower beam affords good radar cover at angles near to the horizon at ranges where clutter is not present. At intermediate ranges the low beam is used with the short pulse to detect targets near the ground to minimise the amount of clutter received whilst the high beam is used with the longer pulse to increase the energy available to detect high flying targets.
Echo signals are not received'until both pulses have been transmitted and so the short pulse is preferably transmitted secondly so that short range data can be received as soon as the short pulse finishes. The pulses are preferably contiguous.
In some embodiments of the invention both the longer and the shorter pulses are used with the higher beam at shorter range which affords more energy to detect targets at high elevation.
In another embodiment of the invention, both the longer and the shorter pulses are used with the lower beam at longer ranges further to increase the energy available to detect distant targets. Thus it will be appreciated from the accompanying specific description wherein
reference is made to the accompanying drawings
that two channels of signal processing only are
required to make maximum use of signals from
four sets of received data.
In order to distinguish between the shorter and
longer pulses for signal processing purposes in a
receiver, the long and short pulses are in the
present example transmitted at different
frequencies whereby they may be received,
filtered and passed through separate receiving
channels.
A system according to one embodiment of the
present invention may comprise an antenna
having a main feed for transmission and reception
and an auxiliary feed for reception only, the main
feed being fed from a radar transmitter via a
duplexer, received signals being passed via the
duplexer to a main receiving channel, a similar
auxiliary receiving channel being coupled to the
auxiliary feed, the transmitter being capable of
transmitting successive radar pulses at
frequencies F1 and F2 and the receiving channels
each including a filter responsive to the
frequencies F1 nd F2, output signals from the
filters being fed to a switch arrangement for
providing output signals to respective channels for
processing in dependence upon range.
An examplary embodiment of the invention will
no.w be described with reference to the
accompanying drawings in which:
Figure 1 is a generally schematic block circuit
diagram of a part of a radar system, and wherein;
Figure 2 is a graph showing the range/altitude
coverage afforded by different antenna
arrangements when fed with radar pulses of
different lengths.
Referring now to Figure 1, the system
comprises an antenna having a reflector 1 and a
pair of feeds associated therewith 2 and 3. The
feed 2 is fed with radar signals from transmitter 4
via a duplexer 5. The transmitter is adapted to
provide in quick succession two contiguous radar
pulses at different frequencies and of different
lengths, the shorter of the two pulses being
transmitted secondly. After the transmission of the
radar pulses, echo signals are received by the
antenna feed 2 which is regarded as the main feed
and passed to a main processor channel on line 6
via duplexer 5. Signals received by the feed 3
which is regarded as the auxiliary feed are passed
via line 7 to an auxiliary processing channel.
Signals on the line 7 are fed in the auxiliary
channel to an R. F. amplifier 8 whilst received
signals on line 6 in the main channel are fed to an
amplifier 9. The amplifiers 8 and 9 are arranged to
feed filters 10 and 11 respectively which are
effective to separate signals at the frequencies F1 and F2.Signals at the frequency F1 from the filters
10 and 11 are fed on lines 12 and 13 respectively
to to a switch unit 14, whilst signals at the frequency
F2 are fed via the filters 10 and 11 respectively on
the lines 1 5 and 16 to the switch unit 1 7. Switch
unit 1 4 feeds a receiver 1 8 including intermediate
frequency processing and amplification circuitry responsive to the frequency F1 whilst the switch unit 1 7 feeds a similar receiver 1 9 responsive to the frequency F2.The receivers 1 8 and 1 9 are arranged to feed signals processors 20 and 21 respectively from which output signals indicative of a target are provided on lines 22 and 23 respectively.
The antenna feed 2 provides echo signals from lower altitude targets than the antenna feed 3 and this is best appreciated by referring now to the graphs shown in Figure 2. It will be assumed for the purposes of the following explanation that a longer radar pulse is transmitted at the frequency F1 which is lower than the frequency F2. In the present enbodiment the radar frequencies for F1 and F2 might be 1 300 MHz and 1340 MHz respectively whilst the pulse length for F1 and F2 might typically be 6M sec. and 1 iu secs. When the main antenna 2 is receiving echos of the longer pulse at F1, a range/altitude graph 24 will obtain as shown in Figure 2.When the main antenna 2 is fed with the shorter pulse at the frequency F2 then a coverage as shown by graph 25 will obtain. If the longer pulse is received at the auxiliary antenna 3, then a much higher altitude coverage will be obtained as shown by the graph 26 in
Figure 2 and if the auxiliary antenna 3 is fed with a shorter pulse at the frequency F2 then coverage will obtain as shown in graph 27.
The switch units 1 4 and 1 7 are arranged so that one or other of the signals fed thereto are routed to the signal processing circuitry and there is also provided the facility for switching the signal off. Operation of the switch units 14 and 17 in dependence upon range is effected as follows. Up to the range 30 nautical miles in the present embodiment of the invention the shorter pulse which is transmitted at frequency F2 only, is fed from the auxiliary feed 3 which has the higher altitude response. Thus it is arranged that no signals are passed through the switch unit 14, whilst switch 1 7 passes signals at the frequency
F2 from the filter 10 which is fed from the auxiliary antenna 3, these signals being passed by the receiver 19 and the signal processor 21 to output terminal 23.
At intermediate ranges, say between 30 and 70 nautical miles, signals at the frequency F2 which is the shorter pulse, are fed from the main antenna 2 via the switch unit 1 7 to provide an output signal on the line 23 and signals at the frequency F1 are fed from the auxiliary antenna 3 via the switch unit 14 to provide an output signal on the terminal 22. At ranges in excess of 70 nautical miles the switch units 14 and 17 are again operated so that no signals are outputed from the switch unit 1 7 at the frequency F2 whereas signals at the frequency F1 and originating from the main antenna 2 are routed via the switch unit 14 the receiver 1 8 and the signal processor 20 to provide an output signal on the terminal 22.
It will be appreciated from the foregoing explanation that two signal processing channels only are provided and that by operating the switch units 14 and 17 in accordance with the range desired, the effective aerial feed and pulse length are selected to provide appropriate outut signals at the terminals 22 and 23.
In an alternative embodiment of the invention, both the longer and the shorter pulses at F1 and
F2 respectively are used with the auxiliary feed at ranges of up to 30 nautical miles. In a further alternative embodiment which may be used in addition to or in combination with the first embodiment, the longer and shorter pulses at frequencies F1 and F2 respectively are used with signals from the main feed 2 at ranges in excess of 70 nautical miles whereby a further increase in the energy available is provided to detect distance targets.
Claims (8)
1. A radar system including an antenna adapted to provide two beams one of which covers a higher elevation than the other and means for producing two successive radar pulses one of which is longer than the other, switch means for selecting in dependence upon range the beam required and for selecting a predetermined pulse length for use therewith so that when receiving signals from short ranges the shorter pulse is used with the higher beam only and when receiving signals from longer ranges the longer pulse is used with the lower beam only and at intermediate ranges the shorter pulse is used with the lower beam whilst the longer pulse is used with the higher beam.
2. A radar system as claimed in claim 1 wherein the shorter pulse is transmitted after the longer pulse.
3. A radar system as claimed in claim 1 or claim 2 wherein the two pulses are contiguous.
4. A radar system as claimed in any preceding claim wherein the longer pulse and the shorter pulse are used with the higher beam at short range thereby to afford more energy to detect targets at high elevation.
5. A radar system as claimed in any preceding claim wherein both the longer and the shorter pulses are used with the lower beam at longer ranges thereby to increase the energy available to detect distant targets.
6. A radar system as claimed in any preceding claim wherein the long and short pulses are transmitted at different frequencies, received echo signals being filtered and passed through separate receiving channels in accordance with frequency.
7. A radar system as claimed in any preceding claim comprising an antenna having a main feed for transmission and reception and an auxiliary feed for reception only the main feed being fed from the radar transmitter via a duplexer, received signals being passed via the duplexerto a main receiving channel, an auxiliary receving channel being coupled to the auxiliary feed, the transmitter being capable of transmitting successive radar pulses at frequencies F1 and F2 and the receiving channels each including a filter responsive to the frequencies F1 and F2, output signals from the filters in each channel being fed to a switch arrangement for providing output signals to respective channels for processing in dependence upon range.
8. A radar system substantially as hereinbefore described with reference to the accompanying drawings.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB7928555A GB2030416B (en) | 1978-09-09 | 1979-08-16 | Radar systems |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB7836243 | 1978-09-09 | ||
GB7928555A GB2030416B (en) | 1978-09-09 | 1979-08-16 | Radar systems |
Publications (2)
Publication Number | Publication Date |
---|---|
GB2030416A true GB2030416A (en) | 1980-04-02 |
GB2030416B GB2030416B (en) | 1982-12-22 |
Family
ID=26268803
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB7928555A Expired GB2030416B (en) | 1978-09-09 | 1979-08-16 | Radar systems |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB2030416B (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0061941A2 (en) * | 1981-03-30 | 1982-10-06 | Allied Corporation | Radar system providing optimized target resolution of both short and long range targets |
WO1990013048A1 (en) * | 1989-04-22 | 1990-11-01 | Cambridge Consultants Limited | System for sensing the approach of a moving missile to a target |
GB2299907A (en) * | 1984-12-10 | 1996-10-16 | Dassault Electronique | Pulse radar |
US7657059B2 (en) * | 2003-08-08 | 2010-02-02 | Lockheed Martin Corporation | Method and apparatus for tracking an object |
-
1979
- 1979-08-16 GB GB7928555A patent/GB2030416B/en not_active Expired
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0061941A2 (en) * | 1981-03-30 | 1982-10-06 | Allied Corporation | Radar system providing optimized target resolution of both short and long range targets |
EP0061941A3 (en) * | 1981-03-30 | 1982-12-01 | The Bendix Corporation | Radar system providing optimized target resolution of both short and long range targets |
GB2299907A (en) * | 1984-12-10 | 1996-10-16 | Dassault Electronique | Pulse radar |
GB2299907B (en) * | 1984-12-10 | 1997-05-14 | Dassault Electronique | Pulse radar apparatus and method |
WO1990013048A1 (en) * | 1989-04-22 | 1990-11-01 | Cambridge Consultants Limited | System for sensing the approach of a moving missile to a target |
US7657059B2 (en) * | 2003-08-08 | 2010-02-02 | Lockheed Martin Corporation | Method and apparatus for tracking an object |
Also Published As
Publication number | Publication date |
---|---|
GB2030416B (en) | 1982-12-22 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
732 | Registration of transactions, instruments or events in the register (sect. 32/1977) | ||
PCNP | Patent ceased through non-payment of renewal fee |
Effective date: 19930816 |