[go: up one dir, main page]

CN100334466C - Shipboard three-dimensional radar and antenna arrangement therefor - Google Patents

Shipboard three-dimensional radar and antenna arrangement therefor Download PDF

Info

Publication number
CN100334466C
CN100334466C CNB2003801077424A CN200380107742A CN100334466C CN 100334466 C CN100334466 C CN 100334466C CN B2003801077424 A CNB2003801077424 A CN B2003801077424A CN 200380107742 A CN200380107742 A CN 200380107742A CN 100334466 C CN100334466 C CN 100334466C
Authority
CN
China
Prior art keywords
channel
input
output
antenna
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.)
Expired - Fee Related
Application number
CNB2003801077424A
Other languages
Chinese (zh)
Other versions
CN1732392A (en
Inventor
尼古拉·D·博罗金
鲍里斯·M·格尔佐夫斯基
瓦莱瑞·I·吉尔尤克
尤里耶·T·科洛米琴科
维克托·T·科尔廖夫
亚历山大·V·洛巴诺夫
阿列克谢·I·涅莫利亚耶夫
维克托·P·奥莱瓦诺夫
维克托·A·帕宁
亚历山大·M·里亚索夫斯基
维克托·D·塔拉索夫
阿尔贝特·V·扎列夫斯基
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.)
FED STATE UNITARY ENTPR STATE
Original Assignee
FED STATE UNITARY ENTPR STATE
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 FED STATE UNITARY ENTPR STATE filed Critical FED STATE UNITARY ENTPR STATE
Publication of CN1732392A publication Critical patent/CN1732392A/en
Application granted granted Critical
Publication of CN100334466C publication Critical patent/CN100334466C/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Images

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
    • G01S13/00Systems 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
    • G01S13/87Combinations of radar systems, e.g. primary radar and secondary radar
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q1/00Details of, or arrangements associated with, antennas
    • H01Q1/27Adaptation for use in or on movable bodies
    • H01Q1/34Adaptation for use in or on ships, submarines, buoys or torpedoes
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q25/00Antennas or antenna systems providing at least two radiating patterns
    • H01Q25/005Antennas or antenna systems providing at least two radiating patterns providing two patterns of opposite direction; back to back antennas
    • 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
    • G01S13/00Systems 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
    • G01S13/02Systems using reflection of radio waves, e.g. primary radar systems; Analogous systems
    • G01S2013/0236Special technical features
    • G01S2013/0272Multifunction radar

Landscapes

  • Engineering & Computer Science (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Computer Networks & Wireless Communication (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Radar Systems Or Details Thereof (AREA)
  • Variable-Direction Aerials And Aerial Arrays (AREA)

Abstract

The present invention relates to a peculiar shipborne radar workstation which comprises two radar communication channels that operate in separated sub-frequency bands, wherein each communication channel is composed of a respective electronic scanning and transmitting receiving antenna array. The antenna arrays are arranged so as to be circumferentially rotatable on a common stable platform, and the antenna arrays are formed so that signals transmitted from the antenna arrays face mutually reverse directions. Each communication channel is provided with an ultra-high frequency transmitter-receiver. The shipborne radar also comprises a forming, processing and signal multiplying device, an information automatic processing device and a device used for the display of the two communication channels.

Description

Boat-carrying 3-D radar and the antenna equipment that is used for it
Technical field
The present invention relates to the radiolocation field, particularly shipborne radar workstation (radar).The radar that is proposed can be used for the detection of aerial and terrain object and the transmission of target indication.
Background technology
Known shipborne radar (BrP No.2177566), wherein in order to increase from the quantity of the pulse of target reflection, emission two or some beams have been proposed, these beams are separated out in the leveling board (horizontal plate on a comer) of corner, and the width of beam is suitable.The deficiency of this judgement is that it does not increase data update rate.
With the immediate analog of disclosed invention (prototype) be the 3-D radar AN/SPS-48E (according to the catalogue 1997-1998 of the naval of world's naval weapon system association's guide (The NavalInstitute Guide to World Naval Weapons Systems)) of USN.Radar AN/SPS-48E represents only to be operated in the single channel workstation of a position of frequency range.Radar AM/SPS-48E rotates by the circumferential motor that utilizes antenna in the leveling board and scans one or one group of beam, and carries out the space inspection in vertical panel (vertical plate).Antenna equipment has hole, slit (slot-hole) structure of waveguide.Carry out and wave (roll) and face upward the stable of bow (pitch) relevant antenna beam pattern by the electronics mode.The operator scheme that depends on radar, emitter produce have height, the corresponding beam of medium or low emissive power.The basic shortcoming of radar AN/SPS-48E is quite low data update rate, and can not detect the target in low-latitude flying.Distinctive deficiency can cause reducing of tracking stability, and the scope of target indication transmission and the minimizing of degree of accuracy.
Summary of the invention
The objective of the invention is to develop a kind of radar workstation, it has the pinpoint accuracy that data update rate, coordinates of targets are measured and the target indication transmits of increase, the sensing range of increase, comprises the undersized target of low-latitude flying.Compare with prototype, distinctive purpose is to realize by the radar with two channel architectures, wherein by two independently channel realize the emission of detectable signal and from the reception of the signal of target reflection.Two frequency channels structurally are identical, and are operated in two frequency subrange places that separate of E band in the common issue RX path.Each channel has the device that transmits and receives of transmit receive antenna, HF signal.Because structurally being provided with two frequency channels adds up and segmenting device, so be provided at two independent operations that separate the radar in the subrange frequency.The antenna that transmits and receives of Radar channel opens toward each other, makes to lead them from the signal of their emissions in relative direction mutually, and transmits and receives antenna and be installed on the general stable frame with the IFF antenna.The abundant mechanically stable of the turning axle of the antenna of Radar channel and IFF system will be eliminated the influence to the radar characteristic of waving of ship.Owing to have the formation of the beam pattern of low secondary lobe (side-lobes) level, realized the pinpoint accuracy that the target indication transmits.Utilize the operation of two frequency channels allow to get rid of seriously invalid in the detection of the aerial target of low-latitude flying, and data update rate has been increased twice.
By electron scanning, utilize two Radar channel to carry out space inspection to the mechanical rotation of antenna in beam in the vertical panel and the leveling board.According in variation, carry out the scanning of vertical panel corresponding to the transmit frequency signal under the specific program of the operator scheme of establishing.Scanning sequence is set order and the various detectable signal that beam is followed.Measure desired degree of accuracy for the energy potential and the scope that realize necessity, use synthetic detectable signal with linear frequency modulation (LFM).Control the control of carrying out recurrence interval, recurrent frequency and power that transmits and kind by display unit and pattern; this control makes emitted energy in the spatial distributions optimization, and the spatial placement that allows to depend on barrier is used the interference protection resource effectively.In order to increase service efficiency, in radar, the great majority in the selection of control, scan control, signal kinds and the disposal route thereof of interaction, applicability and the fault search of automatic realization operation switching, various devices.For same purpose, depend on the problem that workstation is solved at present time durations, the various patterns that the application space is checked, the i.e. algorithm of the formation of beam motion, signal and processing.Agreement cut off from the antenna to the emitter and emitter to opportunity of the connection of " illusory antenna ".
Description of drawings
Fig. 1 has shown the basic device of radar and their mutual relationship.
As shown in Figure 1, radar is made up of following array apparatus in order:
1, the first channel antenna;
2, second channel antenna;
3, the first frequency channel adds up and segmenting device;
4, IFF antenna;
5, multichannel rotation joint portion;
6, guided wave rotation joint portion;
7, driving and stabilising arrangement;
8, the switching device shifter of " illusory antenna " pattern-" antenna " pattern;
9, the second frequency channel adds up and segmenting device;
10, the first channel duplexer;
11, first channel amplifies self-checking device;
12, moving target indicator (MTI);
13, second channel amplifies self-checking device;
14, second channel duplexer;
15, the first channel receiver protective device;
16, the first channels transmit device;
17, restriction and adjustment filtration unit;
18, second channel emitter;
19, second channel receiver protective device;
20, the first channel SHF receiving trap;
21, the first fading channel device;
22, monodrome signal gating device;
23, second-channel attenuation device;
24, the SHF receiving trap of second channel;
25, signal blanking (blanking) device;
26, be used to form the device of linear frequency linearly modulated signal;
27, data representation and mode control device
28, data processing equipment;
29, input and reproducing unit;
30, driving control device.
Embodiment
Antenna equipment have in leveling board rotation and wave with pitching in the framework of mechanically stable, placed the first Radar channel antenna 1, the second Radar channel antenna 2 and the IFF antenna 3 of structural similarity thereon, wherein the first Radar channel antenna 1 and the second Radar channel antenna 2 open by the emitting surface of opposition side.In Fig. 1,7 have shown driving and stabilising arrangement in the position.
Transmit from data representation in the device 26 that is used to form the linear frequency signal and mode control device 27.The linear frequency signal that produces according to scrutiny program reaches device 20 and 24, and it forms device by ultrahigh frequency (SHF) receiver, oscillator and ultra-high frequency signal forms, and further signal arrives emitter 16 and 18.The emitter of first and second frequency channels structurally is identical, and has 3 grades of amplifying circuits.In the first order travelling-wave tube is set, second and the third level use oscillator.The SHF signal is limited by HV (high pressure) pulse and amplifies in amplifying circuit, and the HV pulse is from the high voltage modulator that is included in the emitter.When lacking modulation signal, the amplitron amplifier of second and the third level of transmitter makes the SHF signal pass through with small decay, and it can realize operationally controlling emissive power.
The detectable signal process switch 10 and 14 of the emitter of first and second channels adds up in device 9, through switch 8, rotation joint portion 6, rotation joint portion 5 and arrival antenna equipment, cuts apart the back at this in device 4 and arrives antenna 1 and 2.Hole, planar waveguides slit antenna 1 and 2 is made up of the waveguide scale (ruler) with the transmitting aperture on the narrow wall, its be included in the waveguide power determiner of antenna in forming and be connected, and use the waveguide of the direct coupling mechanism formation of Waveguide coaxial S shape.Discrete Change according to the carrier frequency of each channel provides the electron scanning of the beam in the inspection area in height.Do not transmit signals to air in order to carry out adjustment work, fix on the device 8 that comprises switch and " illusory antenna " approximately and help down, disconnect emitter and emitter chance to the connection of " illusory antenna " from antenna.
Received by antenna 1 and 2 from the radar signal of target reflection, 4 places add up at device, through rotation joint portion 5, rotation joint portion 6, switch 8, device 9, switch 10 and 14 and install 15 and 19, arrive receiving trap 20 and 24.In order to be in the signal that the intermediate frequency conversion receives at receiver, use same oscillator, as converter, it carries out the conversion of the intermediate frequency spectrum in the SHF of transmitting boundary signal.From installing 20 and 24, intermediate-freuqncy signal arrives device 11 and 13, wherein carries out the time adjustment of amplification and the autostable of noise jamming and barrier level.Further, signal arrives device 12, wherein carries out the compensation of passive obstacle and from the signal allocation of the moving target on the bottom beam of inspection area, from its output, signal arrives the input of device 17, and device 17 is used to resist the adjustment filtration of wideband pulse obstacle and composite signal.Directly arrive the input of device 17 from the output of device 11 and 13 and the signal that target reflected from the beam of top, inspection area.Then, signal arrives the sniffer 25 of determining (unequivocal) signal detecting device 22 and signal blanking.In order to express surface condition (the bottom beam of surveyed area), fading channel device 21 and 23 are set, wherein signal and further is sent to device 17 and 25 from device 11.Afterwards, the signal arriving signal detects and reproducing unit 29, and further arrives data processing equipment 28, data presentation device and workstation control model device 27, and other consumer of information.Device 28 is automatic workplaces that the operator carries out target initial input and support.The structure of the expression of radar and mode control device 27 comprises control panel and data representation piece.Carry out rotary mode and stable control by device 30.

Claims (6)

1, a kind of boat-carrying 3-D radar comprises: the first channel antenna (1); IFF antenna (4), its input-output is connected with the input-output of multichannel rotation joint portion (5); The first channel duplexer (10), its output is connected with first input of the first channel ultrahigh frequency SHF receiving trap (20) via the first channel receiver protective device (15), first output of the first channel ultrahigh frequency receiving trap (20) is connected with the input of the first channels transmit device (16), the input of the first channels transmit device (16) is connected with the input of the first channel duplexer (10), and second output of the first channel ultrahigh frequency SHF receiving trap (20) is connected with the input of the first channel amplification coefficient self-checking device (11), the output of the first channel amplification coefficient self-checking device (11) is connected with the input of moving target indicator MTI (12), and moving target indicator (12) is connected with adjustment filter (17) all the time with restriction; Monodrome signal gating device (22) and signal blanker (25), second input of signal blanker (25) is connected with the output of the first fading channel device (21), second output of the first fading channel device (21) is connected with second input of adjusting filter (17) with restriction, the 3rd input of restriction and adjustment filter (17) is connected to second output of the first channel amplification coefficient self-checking device (11), the 3rd output of the first channel amplification coefficient self-checking device (11) is connected with the input of the first fading channel device (21), the output of signal blanker (25) is connected with the input of input with reproducing unit (29) thus, first output of input and reproducing unit (29) is the output of radar, second output is connected with the input of data representation with mode control device (27), and the 3rd output be connected with the input of data processing equipment (28), data processing equipment (28) is connected with the device that is used to form linear frequency modulation signal (26) with mode control device (27) with data representation continuously, first output that is used to form the device (26) of linear frequency modulation signal is connected with second input of the first channel SHF receiving trap (20), it is characterized in that it comprises second channel antenna (2); Drive and stabilising arrangement (7); Driving control device (30); The first frequency channel adds up and segmenting device (3); its first input-output is connected with the first channel antenna (1); its second input-output is connected with second channel antenna (2); and the 3rd input-output rotate joint portion (5) via multichannel; waveguide rotation joint portion (6) and " illusory antenna " pattern-" antenna " mode-changeover device (8); add up with the second frequency channel and to be connected with first input-output of segmenting device (9); the second frequency channel adds up and is connected with the input-output of the first channel duplexer (10) with second input-output of segmenting device (9); with and the 3rd input-output be connected with the input-output of second channel duplexer (14); the output of second channel duplexer (14) is connected with first input of second channel SHF receiving trap (24) via second channel receiver protector (19); first output of second channel SHF receiving trap (24) is connected with the input of second channel receiving trap (18); the output of second channel receiving trap (18) is connected with the input of second channel duplexer (14); and second output of second channel SHF receiving trap (24) is connected with the input of second channel amplification coefficient self-checking device (13); first output of second channel amplification coefficient self-checking device (13) is connected with the input of moving target indicator MTI (12); its second output is connected with the 4th input of adjusting filtration unit (17) with restriction; and the 3rd output be connected with the input of second-channel attenuation device (23); first output of second-channel attenuation device (23) is connected with the 5th input of adjusting filtration unit (17) with restriction; and second output import with the 3rd of signal blanker (25) and be connected; second output that is used to form the device (26) of linear frequency modulation signal thus is connected with second input of second channel SHF receiving trap (24); and second output of data representation and mode control device (27) is connected with the input of driving control device; the output of driving control device is connected with the input of driving and stabilising arrangement, drives with stabilising arrangement mechanically to be connected with multichannel rotation joint portion with waveguide rotation joint portion.
According to the boat-carrying 3-D radar of claim 1, it is characterized in that 2, the first and second Radar channel emitters self have 3 grades of amplifying circuits, and use travelling-wave tube in first cascade place, and second and third level connection place use amplitron.
According to the boat-carrying 3-D radar of claim 1, it is characterized in that 3, the first and second Radar channel ultrahigh frequency receiving traps form device by SHF receiver, oscillator and ultra-high frequency signal and form.
4, according to the boat-carrying 3-D radar of claim 1, it is characterized in that, agreement cut off from the antenna to the emitter and emitter to opportunity of the connection of " illusory antenna ".
5, a kind of antenna equipment that is used for boat-carrying 3-D radar, comprise the reception and the emitting antenna that are installed on the framework, framework can rotate by circumference in leveling board, it is characterized in that, the reception and the emitting antenna of second similar are set, it is operated in another sub-band, and receive with first and emitting antenna combines and is installed on this framework, make transmitting of antenna be directed to mutually opposite direction, drive thus and be used for mechanically stable and wave and pitching and the device that rocks, and be stabilized in waving in the situation of establishing antenna.
According to the antenna equipment of claim 5, it is characterized in that 6, these antenna is disposed in N line level in the visual field of Waveguide slot transmitter, each Waveguide slot transmitter is connected with the waveguide of S shape via the Waveguide coaxial coupling mechanism.
CNB2003801077424A 2003-10-14 2003-10-14 Shipboard three-dimensional radar and antenna arrangement therefor Expired - Fee Related CN100334466C (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
PCT/RU2003/000437 WO2005038484A1 (en) 2003-10-14 2003-10-14 Shipboard three-dimensional radar and an antenna arrangement therefor

Publications (2)

Publication Number Publication Date
CN1732392A CN1732392A (en) 2006-02-08
CN100334466C true CN100334466C (en) 2007-08-29

Family

ID=34464995

Family Applications (1)

Application Number Title Priority Date Filing Date
CNB2003801077424A Expired - Fee Related CN100334466C (en) 2003-10-14 2003-10-14 Shipboard three-dimensional radar and antenna arrangement therefor

Country Status (2)

Country Link
CN (1) CN100334466C (en)
WO (1) WO2005038484A1 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2758484C2 (en) * 2020-03-24 2021-10-28 Федеральное государственное казенное военное образовательное учреждение высшего образования "Военный учебно-научный центр Военно-Морского Флота "Военно-морская академия имени Адмирала флота Советского Союза Н.Г. Кузнецова" Shipboard vhf receiving antenna system

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7609198B2 (en) * 2007-05-21 2009-10-27 Spatial Digital Systems, Inc. Apparatus and method for radar imaging by measuring spatial frequency components
JP5558943B2 (en) * 2010-07-06 2014-07-23 古野電気株式会社 Slot array antenna and radar device

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
SU943933A1 (en) * 1980-10-20 1982-07-15 Предприятие П/Я А-1819 Device for stabilizing vehicle-mounted object
US4609083A (en) * 1983-03-31 1986-09-02 Stuhler William B Reactive attitude stabilization system
US5864314A (en) * 1996-11-15 1999-01-26 Honda Giken Kogyo Kabushiki Kaisha FM radar system
RU2184411C2 (en) * 1999-04-12 2002-06-27 Научно-исследовательский институт "Стрела" Antenna system and aperture power distribution control device

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2155354C1 (en) * 1999-11-04 2000-08-27 Закрытое акционерное общество "Морские комплексы и системы" Radar system

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
SU943933A1 (en) * 1980-10-20 1982-07-15 Предприятие П/Я А-1819 Device for stabilizing vehicle-mounted object
US4609083A (en) * 1983-03-31 1986-09-02 Stuhler William B Reactive attitude stabilization system
US5864314A (en) * 1996-11-15 1999-01-26 Honda Giken Kogyo Kabushiki Kaisha FM radar system
RU2184411C2 (en) * 1999-04-12 2002-06-27 Научно-исследовательский институт "Стрела" Antenna system and aperture power distribution control device

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2758484C2 (en) * 2020-03-24 2021-10-28 Федеральное государственное казенное военное образовательное учреждение высшего образования "Военный учебно-научный центр Военно-Морского Флота "Военно-морская академия имени Адмирала флота Советского Союза Н.Г. Кузнецова" Shipboard vhf receiving antenna system

Also Published As

Publication number Publication date
CN1732392A (en) 2006-02-08
WO2005038484A1 (en) 2005-04-28

Similar Documents

Publication Publication Date Title
CN101013159B (en) Object Detection Devices and Systems
EP0396611B1 (en) Vehicular anticollision radar system
US7737879B2 (en) Split aperture array for increased short range target coverage
EP2342581B1 (en) Clutter reduction in detection systems
US7423578B1 (en) Split aperture array for increased short range target coverage
US8912950B2 (en) Interference mitigation in through the wall radar
US8217827B2 (en) Radar method and apparatus suitable for use in multipath environments
US6218979B1 (en) Wide area time domain radar array
US7486224B2 (en) Microwave and millimeter frequency bistatic radar tracking and fire control system
Robertson Practical ESM analysis
RU2444755C1 (en) Method for detection and spatial localisation of air objects
CN112782697A (en) Unmanned aerial vehicle airborne anti-collision radar system and working method
KR20190006561A (en) Low-flying Unmanned Aerial Vehicle and Object Tracking Radar System
RU2444754C1 (en) Method for detection and spatial localisation of air objects
US3879732A (en) Multi-directional barrage jamming system
US2687520A (en) Radar range measuring system
CN108196250B (en) Continuous wave radar system and method for low-altitude small target detection
CN105652245B (en) A kind of solid state pulse compression radar width is from covering method
CN100334466C (en) Shipboard three-dimensional radar and antenna arrangement therefor
CN104914430B (en) Array radar system adaptively selecting transmitting array elements according to target distance
RU2254593C1 (en) Shipboard three-dimensional radar station and antenna arrangement for it
US20220229175A1 (en) Coherent, Multi-Static Radar System, In Particular For Use In A Vehicle
RU2444756C1 (en) Detection and localisation method of air objects
RU2444753C1 (en) Radio monitoring method of air objects
RU2285939C1 (en) Method for controlling airspace, irradiated by external radiation sources, and radiolocation station for realization of said method

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
C14 Grant of patent or utility model
GR01 Patent grant
CF01 Termination of patent right due to non-payment of annual fee
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20070829