CN109190303A - Middle short range search radar emits signal width pulse width ratio design method - Google Patents
Middle short range search radar emits signal width pulse width ratio design method Download PDFInfo
- Publication number
- CN109190303A CN109190303A CN201811198256.2A CN201811198256A CN109190303A CN 109190303 A CN109190303 A CN 109190303A CN 201811198256 A CN201811198256 A CN 201811198256A CN 109190303 A CN109190303 A CN 109190303A
- Authority
- CN
- China
- Prior art keywords
- wide
- pulse
- pulse width
- width
- width ratio
- 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
- G06—COMPUTING; CALCULATING OR COUNTING
- G06F—ELECTRIC DIGITAL DATA PROCESSING
- G06F30/00—Computer-aided design [CAD]
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02A—TECHNOLOGIES FOR ADAPTATION TO CLIMATE CHANGE
- Y02A90/00—Technologies having an indirect contribution to adaptation to climate change
- Y02A90/10—Information and communication technologies [ICT] supporting adaptation to climate change, e.g. for weather forecasting or climate simulation
Abstract
The present invention discloses a kind of middle short range search radar transmitting signal width pulse width ratio design method, and this method is for middle short range search radar transmitting signal pulse repetition period, the design of width pulse width.The present invention, which is solved the problems, such as over, finds wide, narrow pulse width by heuristic method, by the derivation to wide, burst pulse detection range, gives width, narrow pulse width ratio and emits signal dutyfactor α, is connected coefficient gamma, σIt is small, σGreatlyRelationship, can directly calculate wide, narrow pulse width ratio value range.Compared to conventional heuristic method, the method in the present invention can directly find out optimal wide, narrow pulse width ratio.
Description
Technical field
The invention belongs to Radar Technology fields, and in particular to middle short range search radar transmission signal parameters design is applied to
Middle short range search radar transmitting signal width pulse width design, consequently facilitating quickly reasonably finding out optimal width pulse width
Than.
Background technique
Middle short range search radar in order to solve the contradiction of minimum detectable range and maximum probe power, often select by transmitting signal
The pulse signal of wide, narrow two kinds of pulse widths, wide pulse signal are responsible for the detection to far field airspace, and narrow pulse signal is responsible for close
The detection in area airspace.The echo-signal of two kinds of pulse widths, which shares, receives the period, and the timing for emitting signal is as shown in Figure 1.
Since broad pulse and burst pulse share reception interval, in order to distinguish the echo of two kinds of pulses, often using different
Signal form and signal frequency.After wide, narrow pulse signal, to solve that different RCS targets are wide, burst pulse detection range have
A series of problems, such as effect connection problem emits signal pulse repetition period select permeability, and wide, narrow pulse width designs.
It is provided there is presently no pertinent literature and how to select wide, narrow pulse width ratio, correlative technology field is to pass through examination
The method of spy provides the design of width pulse width.Heuristic method obtains transmitting signal pulse according to the power of radar first and repeats week
Phase and broad pulse width find out narrow pulse width according to minimum detectable range, then calculate width arteries and veins within the scope of detection target RCS
Radar power coverage area is rushed, if width pulse detection distance can not be connected, width pulse width is readjusted, so recycles
Until finding the width pulse width met the requirements.Heuristic method is computationally intensive, low efficiency, the width arteries and veins met the requirements found
It rushes width not optimize, the present invention gives width pulse width ratio value range by the derivation of equation, chooses ratio
Optimal width pulse width ratio can be obtained in maximum value.
Summary of the invention
Technical problems to be solved
In order to avoid the shortcomings of the prior art, the present invention proposes a kind of middle short range search radar transmitting signal width arteries and veins
It rushes width and compares design method.
Technical solution
A kind of middle short range search radar transmitting signal width pulse width ratio design method, it is characterised in that steps are as follows:
Step 1: according to duty cycle alpha, linking coefficient gamma, radar detection target RCS minimum value σIt is smallWith maximum value σGreatly, calculate
The value range of broad pulse and burst pulse time width ratio beta:
Step 2: β takes the maximum value met the requirements, calculates σGreatlyCorresponding radar horizon RMax_ wide:
Wherein, PtFor emission peak power, GtFor transmitter antenna gain (dBi), GrFor receiving antenna gain, λ is wavelength, and σ is mesh
Specular cross section is marked, k is Boltzmann constant, D0It (1) is detecting factor, TsTo receive system equivalent noise temperature, LsTo be
System loss, T are wave beam residence time;
Step 3: according to RMax_ wideCalculate pulse repetition period t:
RMax_ wide≈t(1-α)×150×106
Step 4: it is wide that width pulse being found out by duty cycle alpha, pulse repetition period t, broad pulse and burst pulse time width ratio β value
Degree:
Beneficial effect
A kind of middle short range search radar proposed by the present invention emits signal width pulse width ratio design method, and what is had has
Beneficial effect is:
1) formula (17) gives width, narrow pulse width ratio and emits signal dutyfactor α, is connected coefficient gamma, σIt is small, σGreatly's
Relationship can directly calculate wide, narrow pulse width ratio value range;
2) it solves the problems, such as over and wide, narrow pulse width is found by heuristic method;
3) radar emission signal parameter can more reasonably be designed by formula (5), formula (10), formula (17).
Detailed description of the invention
Fig. 1 emits signal timing diagram
Fig. 2 wide, burst pulse investigative range schematic diagram
Specific embodiment
Now in conjunction with embodiment, attached drawing, the invention will be further described:
According to radar equation:
Wherein:
Pt: emission peak power
τ: fire pulse width
Gt: transmitter antenna gain (dBi)
Gr: receiving antenna gain
λ: wavelength
σ: specular cross-section
Ii: accumulation improvement factor
K: Boltzmann constant
Ts: receive system equivalent noise temperature
D0(1): detecting factor
Ls: system loss
Assuming that:
Broad pulse and burst pulse time width ratio are as follows: β,
Pulse repetition period are as follows: t
Wave beam residence time are as follows: T
Emit signal dutyfactor are as follows: α,
Then:
By formula (2), formula (3) substitutes into formula (1), can obtain:
By formula (2), formula (4) substitutes into formula (1), can obtain:
If:
Then:
As shown in Figure 2, since narrow pulse signal time width is small, maximum detectable range when broad pulse detection range is not fuzzy
Are as follows:
RMax_ wide≈t(1-α)×150×106 (10)
Burst pulse distance measurement, which is greater than, is equal to transmitting pulse signal blind area, therefore:
RMax_ is narrow≥tα×150×106 (11)
It is equal to transmitting pulse signal detection since there are directional diagram mismatch loss, burst pulse distance measurement is greater than in practice
γ times of blind area, γ are defined as linking coefficient, and the value of γ is determined by system parameters, therefore:
RMax_ is narrow≥tαγ×150×106 (12)
Radar detection object generally comprises the typical targets such as fixed wing aircraft, armed helicopter, unmanned plane, cruise missile,
The RCS of target is generally by 0.01m2To 2m2It differs, some radars require the RCS range of detection target wider.Ideal signal shape
Formula, may be implemented effective detection to all typical targets, and wide, burst pulse detection range can also be connected well.This method is logical
The derivation of equation is crossed, wide, the narrow pulse width ratio value range in the case where setting RCS ambit is given, solves over and pass through
Heuristic method finds out wide, narrow pulse width conventional method.
Assuming that the range of radar detection target RCS is σIt is small~σGreatlyIf to be met wide, narrow using same group of transmitting signal
The linking of pulse detection distance it is necessary to simultaneously meet the following conditions: σGreatlyThe detection range of target needs to meet
RMax_ wide≈t(1-α)×150×106, σIt is smallThe detection range of target need to meet RMax_ is narrow≥tα×150×106, will be public
Formula (8) substitutes into formula (10), and formula (9) are substituted into formula (12), therefore:
It can be derived by formula (13):
Formula (15) substitution formula (14) can be derived:
It can be derived by formula (16):
By formula (5) and formula (17) it follows that
Emit under signal dutyfactor α, linking coefficient gamma certain situation, σIt is smallIt is smaller, σGreatlyBigger, β is smaller, RMax_ wideIt is smaller.Cause
This, the range of radar detection target RCS is bigger, and the detection range of big target is closer, this is often that we are undesirable;β is got over
Greatly, RMax_ wideBigger, β takes the maximum value met the requirements.
This method gives middle short range search radar by the derivation of equation and emits wide signal, narrow pulse width ratio and transmitting
Signal dutyfactor α, linking coefficient gamma, σIt is small, σGreatlyRelationship, can directly calculate wide, narrow pulse width ratio value range.It can
Emit signal pulse repetition period, width pulse width to rationally design.Specific implementation step is as follows:
1) radar emission signal dutyfactor, linking coefficient and detection target RCS range are determined, that is, determines duty cycle alpha, rank
Meet coefficient gamma, σIt is smallAnd σGreatly;
2) according to the above parameter, β value range is calculated by formula (17);
3) β takes the maximum value met the requirements, calculates σ according to formula (5)GreatlyCorresponding radar horizon RMax_ wide;
4) pulse repetition period t can be found out according to formula (10);
5) according to formula (3), (4) by duty cycle alpha, pulse repetition period t, β value finds out width pulse width.
Claims (1)
1. a kind of middle short range search radar emits signal width pulse width ratio design method, it is characterised in that steps are as follows:
Step 1: according to duty cycle alpha, linking coefficient gamma, radar detection target RCS minimum value σIt is smallWith maximum value σGreatly, calculate wide arteries and veins
The value range of punching and burst pulse time width ratio beta:
Step 2: β takes the maximum value met the requirements, calculates σGreatlyCorresponding radar horizon RMax_ wide:
Wherein, PtFor emission peak power, GtFor transmitter antenna gain (dBi), GrFor receiving antenna gain, λ is wavelength, and σ has for target
Reflective surface area is imitated, k is Boltzmann constant, D0It (1) is detecting factor, TsTo receive system equivalent noise temperature, LsFor system damage
Consumption, T are wave beam residence time;
Step 3: according to RMax_ wideCalculate pulse repetition period t:
RMax_ wide≈t(1-α)×150×106
Step 4: width pulse width is found out by duty cycle alpha, pulse repetition period t, broad pulse and burst pulse time width ratio β value:
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201811198256.2A CN109190303B (en) | 2018-10-15 | 2018-10-15 | Method for designing width-to-width pulse width ratio of medium-short range search radar transmitted signal |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201811198256.2A CN109190303B (en) | 2018-10-15 | 2018-10-15 | Method for designing width-to-width pulse width ratio of medium-short range search radar transmitted signal |
Publications (2)
Publication Number | Publication Date |
---|---|
CN109190303A true CN109190303A (en) | 2019-01-11 |
CN109190303B CN109190303B (en) | 2023-04-07 |
Family
ID=64944989
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201811198256.2A Active CN109190303B (en) | 2018-10-15 | 2018-10-15 | Method for designing width-to-width pulse width ratio of medium-short range search radar transmitted signal |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN109190303B (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN110082729A (en) * | 2019-05-17 | 2019-08-02 | 成都锦江电子系统工程有限公司 | Weather radar mends blind smoothing processing system and method |
CN110703270A (en) * | 2019-10-08 | 2020-01-17 | 歌尔股份有限公司 | Depth module ranging method and device, readable storage medium and depth camera |
CN111896971A (en) * | 2020-08-05 | 2020-11-06 | 上海炬佑智能科技有限公司 | TOF sensing device and distance detection method thereof |
CN112068112A (en) * | 2020-07-30 | 2020-12-11 | 西安电子科技大学 | Wide-narrow pulse angle measurement method |
Citations (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP2309289A1 (en) * | 2009-09-25 | 2011-04-13 | Thales | Method for separating interleaved radar pulses sequences |
CN102998658A (en) * | 2012-12-03 | 2013-03-27 | 电子科技大学 | Wide and narrow orthogonal pulse compensation method for pulse radar |
CN103064065A (en) * | 2012-12-17 | 2013-04-24 | 西安电子工程研究所 | Waveform design for double-cycle pinch-off type pseudo-random code and signal processing method for echo |
JP2015055573A (en) * | 2013-09-12 | 2015-03-23 | 株式会社東芝 | Radar device |
CN104833965A (en) * | 2015-05-25 | 2015-08-12 | 扬州宇安电子科技有限公司 | Radar beacon machine and diversity radar signal processing method thereof |
CN106940442A (en) * | 2017-03-15 | 2017-07-11 | 西北大学 | A kind of high speed missile-borne radar waveform design method |
CN106950552A (en) * | 2017-04-05 | 2017-07-14 | 邓勇 | A kind of pulse compression radar indifference mends blind correction method |
CN107121674A (en) * | 2016-08-31 | 2017-09-01 | 零八电子集团有限公司 | Adaptive strain waveform switch tracking mesh calibration method |
-
2018
- 2018-10-15 CN CN201811198256.2A patent/CN109190303B/en active Active
Patent Citations (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP2309289A1 (en) * | 2009-09-25 | 2011-04-13 | Thales | Method for separating interleaved radar pulses sequences |
CN102998658A (en) * | 2012-12-03 | 2013-03-27 | 电子科技大学 | Wide and narrow orthogonal pulse compensation method for pulse radar |
CN103064065A (en) * | 2012-12-17 | 2013-04-24 | 西安电子工程研究所 | Waveform design for double-cycle pinch-off type pseudo-random code and signal processing method for echo |
JP2015055573A (en) * | 2013-09-12 | 2015-03-23 | 株式会社東芝 | Radar device |
CN104833965A (en) * | 2015-05-25 | 2015-08-12 | 扬州宇安电子科技有限公司 | Radar beacon machine and diversity radar signal processing method thereof |
CN107121674A (en) * | 2016-08-31 | 2017-09-01 | 零八电子集团有限公司 | Adaptive strain waveform switch tracking mesh calibration method |
CN106940442A (en) * | 2017-03-15 | 2017-07-11 | 西北大学 | A kind of high speed missile-borne radar waveform design method |
CN106950552A (en) * | 2017-04-05 | 2017-07-14 | 邓勇 | A kind of pulse compression radar indifference mends blind correction method |
Non-Patent Citations (4)
Title |
---|
何建新等: "全固态天气雷达组合脉冲发射模式的研究与设计", 《高原气象》 * |
张朝霞等: "利用组合脉冲解决超宽带雷达中探测盲区问题", 《系统工程与电子技术》 * |
赵岩等: "截断式压缩脉冲减小雷达盲区的性能分析", 《现代电子技术》 * |
陈旭波等: "提高某雷达探测距离的可行性分析及工程实现方案", 《空军雷达学院学报》 * |
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN110082729A (en) * | 2019-05-17 | 2019-08-02 | 成都锦江电子系统工程有限公司 | Weather radar mends blind smoothing processing system and method |
CN110082729B (en) * | 2019-05-17 | 2021-05-18 | 成都锦江电子系统工程有限公司 | Processing method of weather radar blind-complementing smoothing processing system |
CN110703270A (en) * | 2019-10-08 | 2020-01-17 | 歌尔股份有限公司 | Depth module ranging method and device, readable storage medium and depth camera |
CN110703270B (en) * | 2019-10-08 | 2022-02-22 | 歌尔光学科技有限公司 | Depth module ranging method and device, readable storage medium and depth camera |
CN112068112A (en) * | 2020-07-30 | 2020-12-11 | 西安电子科技大学 | Wide-narrow pulse angle measurement method |
CN111896971A (en) * | 2020-08-05 | 2020-11-06 | 上海炬佑智能科技有限公司 | TOF sensing device and distance detection method thereof |
CN111896971B (en) * | 2020-08-05 | 2023-12-15 | 上海炬佑智能科技有限公司 | TOF sensing device and distance detection method thereof |
Also Published As
Publication number | Publication date |
---|---|
CN109190303B (en) | 2023-04-07 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN109190303A (en) | Middle short range search radar emits signal width pulse width ratio design method | |
US20240103158A1 (en) | Radar system to track low flying unmanned aerial vehicles and objects | |
CN106990391B (en) | Low Altitude Target Detection wideband radar system and array optimization method based on pitching MIMO | |
US6639546B1 (en) | Radar system in which range ambiguity and range eclipsing are reduced by frequency diversity and alternation of pulse periodicity | |
CN108469607B (en) | Unmanned aerial vehicle detection radar angle measurement method based on frequency scanning antenna | |
CN104977567B (en) | A kind of adaptive launching beam forming method of OFDM monopulse radars | |
CN110068806A (en) | A kind of short distance gapless coverage radar monitoring system of unattended station circumference security protection | |
RU2627958C1 (en) | Method for forming direction diagram by digital antenna array | |
CN109212489A (en) | A kind of fuzzy clutter suppression method of the FDA-MIMO radar based on false impulse | |
US3500395A (en) | Forest terrain search radar method and apparatus | |
US8368583B1 (en) | Aircraft bird strike avoidance method and apparatus using axial beam antennas | |
RU2694891C1 (en) | Method for operation of a pulse-doppler on-board radar station of a fighter while ensuring energy security of its operation for emission | |
CN108614267A (en) | A kind of Anticollision Radar design method based on 77GHz millimeter-wave technologies | |
Matuszewski | Jamming efficiency of land-based radars by the airborne jammers | |
WO2021087706A1 (en) | Radar system, movable platform and radar system control method | |
CN107490791A (en) | A kind of conformal array airborne radar clutter suppression method based on MIMO systems | |
CN206411265U (en) | A kind of double mode radar | |
Colpitts et al. | Harmonic radar for insect flight pattern tracking | |
Van Caekenberghe et al. | A 94 GHz OFDM frequency scanning radar for autonomous landing guidance | |
Madhupriya et al. | Implementation of compressed wave pulsed radar altimeter in signal processing | |
George et al. | Modelling and performance evaluation of ground based monostatic radar surveillance system | |
CN116047462B (en) | Method and device for selecting optimal array element number and array element spacing of end-shooting array airborne radar | |
EP0647359B1 (en) | Airport surveillance radar system for microburst detection | |
Tang et al. | Non-cooperative Bistatic Radar Countermeasures Based on the Joint Design of Radar Waveforms and Mismatched Filters | |
Hızal et al. | Pulsed FMCW waveform design for LPI radars based on stretch processing |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PB01 | Publication | ||
PB01 | Publication | ||
SE01 | Entry into force of request for substantive examination | ||
SE01 | Entry into force of request for substantive examination | ||
GR01 | Patent grant | ||
GR01 | Patent grant |