CN109188374A - Complicated radar overall pulse number production method based on most prepulse - Google Patents

Complicated radar overall pulse number production method based on most prepulse Download PDF

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CN109188374A
CN109188374A CN201810823641.5A CN201810823641A CN109188374A CN 109188374 A CN109188374 A CN 109188374A CN 201810823641 A CN201810823641 A CN 201810823641A CN 109188374 A CN109188374 A CN 109188374A
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pulse
prepulse
radar
radar signal
toa
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CN109188374B (en
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姚金宝
肖鹏
赵亮
刘小亮
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CETC 2 Research Institute
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    • 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
    • G01S7/00Details of systems according to groups G01S13/00, G01S15/00, G01S17/00
    • G01S7/02Details of systems according to groups G01S13/00, G01S15/00, G01S17/00 of systems according to group G01S13/00
    • G01S7/40Means for monitoring or calibrating
    • G01S7/4052Means for monitoring or calibrating by simulation of echoes

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  • Engineering & Computer Science (AREA)
  • Computer Networks & Wireless Communication (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Radar Systems Or Details Thereof (AREA)

Abstract

The present invention relates to technical field of system simulation, disclose a kind of complicated radar overall pulse number production method based on most prepulse.Including following procedure: first arrival pulse in radar signal pulse sequence being defined as the radar signal most prepulse, finds the radar signal most prepulse reached at first in simulated scenario;The describing word parameter for reaching radar signal most prepulse at first is saved in interlaced pulse list to be output, calculates and generates interlaced pulse;Update the forward position arrival time of radar signal most prepulse;For Radar Signal Transmission delay time, the forward position arrival time of radar signal most prepulse is corrected;Update the PDW parameter of radar signal most prepulse;Dynamic, which has been calculated, helps pulse digit generation.Whether the present invention has comprehensively considered radar antenna scanning and has generated to pulse and influence to pulse arrival time of the influence of impulse amplitude size, electromagnetic wave space propagation delay time, has the characteristics that scalability is strong, simulation fidelity is high, arithmetic speed is fast.

Description

Complicated radar overall pulse number production method based on most prepulse
Technical field
The present invention relates to technical field of system simulation, especially a kind of complicated radar overall pulse based on most prepulse Digital production method.
Background technique
The dependence to environment is trained due to the complexity and electronic counter-measures equipment of modern battlefield electromagnetic environment, it is necessary to Realize the radar signal scenario simulation of complicated system, different closenesses.Current radar signal waveform modeling pattern mainly has feature Parameter mode and two kinds of pulse train mode.Wherein, characteristic parameter mode is according to radar signal pattern, by each emulation beat All pulses that interior every radar signals generate are described by characteristic parameter, which computationally has super real-time Advantage, but it is only capable of the emulation of support function grade, verisimilitude is poor;And pulse train mode can be realized to true interlaced pulse sequence Realistic simulation is carried out, pulse grade can be supported to emulate, but the modeling pattern can generate a large amount of overall pulse data, and can dynamic realtime Increase, sort algorithm is complicated, computationally intensive, it is difficult to simulate generation in real time by business computer, often need through DSP come real It is existing.
In view of the above problems, currently having also been proposed arteries and veins group parameter mode, which is a kind of classified statistic description side Formula, all pulses that every radar signals in each emulation beat generate are respectively seen as one group by it has general pulse characteristic Signal, its main feature is that every radar signals group intrinsic parameter does not change, and carrier frequency, repetition interval and pulsewidth etc. between group and group Characteristic parameter is alterable.The modeling pattern performance is between characteristic parameter mode and pulse train mode, due to thunder in organizing It is accordingly to be regarded as general pulse up to signal, so the realization of its sort algorithm is relatively simple, but since the limitation of emulation beat (is difficult to Reach Microsecond grade), it can not support the overall pulse simulation of the complicated system signal such as frequency agility, frequency hopping.
In addition, existing radar signal waveform modeling pattern majority does not consider the delay of radar signal space propagation to overall pulse The influence of generation causes the cross pulse verisimilitude generated not good enough.
Therefore, currently in terms of the multi-section radar overall pulse number of complicated system difference closeness generates research, there are still The problems such as sort algorithm is complicated, computationally intensive, verisimilitude is not good enough, needs continuous exploratory development.
Summary of the invention
The technical problems to be solved by the present invention are: in view of the above problems, provide a kind of based on most prepulse Complicated radar overall pulse number production method.
The technical solution adopted by the invention is as follows: a kind of complicated radar overall pulse number based on most prepulse generates Method specifically includes following procedure: step 1, first arrival pulse in radar signal pulse sequence being defined as the radar Signal most prepulse finds the radar signal most prepulse reached at first in simulated scenario;Step 2, radar letter will be reached at first The describing word parameter of number most prepulse is saved in interlaced pulse list to be output, is calculated and is generated interlaced pulse;Step 3, more The forward position arrival time of new radar signal most prepulse;Step 4, for Radar Signal Transmission delay time, radar signal is corrected The forward position arrival time of most prepulse;Step 5, the PDW parameter of radar signal most prepulse is updated;Step 6, dynamic, which calculates, completes Overall pulse is digitally generated.
Further, the detailed process of the step 1 are as follows: step 11, first in radar signal pulse sequence is arrived The most prepulse of the radar signal is defined as up to pulse, the describing word parameter of the most prepulse includes that the forward position of most prepulse is arrived Up to time TOAi, carrier frequency RFi, pulse repetition period PRIi, pulse width PWi, impulse amplitude PAi, wherein i=0,1 ..., ∞, It is the number of radar signal;Step 12, in calculating simulation scene all radar signals most prepulse forward position arrival time TOAi, Seek the smallest forward position arrival time TOAj(j ∈ { 0,1 ..., ∞ }), corresponding radar signal j is the radar signal reached at first Most prepulse.
Further, in the step 2, the forward position arrival time TOA of radar signal j most prepulsei, carrier frequency RFi, pulse Repetition period is PRIi, pulse width PWi, impulse amplitude PAiIt is saved among interlaced pulse list to be output, completes TOAj All interlaced pulses before moment, which calculate, to be generated.
Further, the detailed process of the step 3 are as follows: step 31, according toWherein, k is current PRF number, when k ∈ { 0,1 ..., ∞ }, k=0 pair Answer the most prepulse of radar signal j;TOAJ, 0The forward position arrival time of pulse, i.e. radar signal j may be reached for the 0th most The forward position arrival time TOA of prepulsej;TOAJ, k+1、TOAJ, kWhen respectively kth, the k+1 forward positions that may reach pulse reach Between;PRIJ, kFor the time interval between kth, the k+1 pulse that may be reached;Persistently iterative calculation radar signal j is next can The forward position arrival time TOA for the pulse that can be reachedJ, k+1;Step 32, the TOA of calculating is verifiedJ, k+1Whether iterated conditional is met, when When radar detection performance is tracking, stopping criterion for iteration is
TOAJ, k< TOAJ, k+1,
When radar detection performance is that circle is swept, stopping criterion for iteration is
When radar detection performance is fan sweeping, stopping criterion for iteration is
Or
Wherein, TjFor radar antenna scan period, W corresponding to radar signal jjIt is wide for wave beam corresponding to radar signal j Degree, aJ, 1For fan sweeping start angle, a corresponding to radar signal jJ, 2For fan sweeping termination point corresponding to radar signal j, until Meet stopping criterion for iteration, obtains the forward position arrival time of updated radar signal most prepulse.
Further, the detailed process of the step 4 are as follows: calculate Radar Signal Transmission delay time td=S/c × 103, S For the distance between radar and radar detection target, c is the light velocity, by the forward position arrival time of radar signal most prepulse plus biography Defeated delay time obtains the forward position arrival time of revised radar signal most prepulse.
Further, in the step 5, the PDW parameter of the update includes carrier frequency RFj, pulse repetition period PRIj, arteries and veins Rush width PWj, impulse amplitude PAj, the renewal process that the frequency carries is RFj'=RFj+ Δ RF × Rand (- 1,1), the pulse The renewal process of repetition period is PRIj'=PRIj+ Δ PRI × Rand (- 1,1), the pulse width PWjIt is constant, the pulse The renewal process of amplitude is
Wherein, TOA 'j, RFj′、PRIj', PWj′、PAj' be respectively updated radar signal j most prepulse forward position Arrival time, carrier frequency, pulse repetition period, pulse width, impulse amplitude, RFj、PRIj, PWj、PAjThunder before respectively updating Up to the carrier frequency of signal j, pulse repetition period, pulse width, impulse amplitude, Rand (- 1,1) indicates to generate in [- 1,1] range Random number, PattenFor radar signal, signal power decays in free space transmission, and S is between radar and radar detection target Distance;Y (x) indicates radar directional pattern data, x ∈ [- 180 °, 180 °].
In conclusion by adopting the above-described technical solution, the beneficial effects of the present invention are: most preceding arteries and veins that the present invention uses Rushing algorithm is a kind of pulse grade emulation, is digitally generated for multi-section complexity radar signal overall pulse, technical side of the invention Case comprehensively considered radar antenna scanning whether pulse is generated and the influence of impulse amplitude size, electromagnetic wave space transmission when Prolong the influence to pulse arrival time, compared with traditional algorithm, with scalability is strong, simulation fidelity is high, arithmetic speed is fast The features such as.It is specific as follows:
A) scalability is strong: the overall pulse that the algorithm is applicable to various complicated radar signals is digitally generated, and can Quickly upgrade the algorithm to be digitally generated with the overall pulse for being suitable for the emerging new system radar signal in battlefield.The algorithm can refer to The detailed process of step 5 is additionally increased by way of similar play with building blocks it is not necessary to modify entire algorithm process logic Add the processing logic branch of corresponding radar signal pattern (pattern including the emerging new system radar signal in battlefield), to update The PDW parameter of corresponding radar signal most prepulse realizes that the overall pulse of various complicated radar signals is digitally generated.
B) simulation fidelity is high: the algorithm introduces whether radar antenna scanning produces pulse by " step 3 and step 5 " Raw and impulse amplitude size influence, has modified electromagnetic wave space propagation delay time to pulse arrival time by " step 4 " It influences, the overall pulse and the overall pulse consistency in true battlefield surroundings for generating emulation are higher.
C) arithmetic speed is fast: for high pulse densities battlefield surroundings (in the battlefield surroundings containing 3 radar signals, Wherein the pulse repetition period of radar signal 1,2,3 is respectively 2 μ s, 3 μ s, 5 μ s, and impulse density is about 103.3 ten thousand pulse/secs) Overall pulse is digitally generated, and (Intel (R) Core (TM) 2Quad CPU, Q9650@3.00Hz) is run on general commercial computer The algorithm is tested, by repeatedly calculating time-consuming test and statistics averaging to the algorithm, obtains every full arteries and veins for calculating and generating 80ms Punching, about need time-consuming 13.5ms, the test result show the algorithm for overall pulse be digitally generated have the characteristics that it is super real-time.
Detailed description of the invention
Fig. 1 is the flow diagram of the complicated radar overall pulse number production method of the invention in most prepulse.
Specific embodiment
All features disclosed in this specification or disclosed all methods or in the process the step of, in addition to mutually exclusive Feature and/or step other than, can combine in any way.
Any feature disclosed in this specification unless specifically stated can be equivalent or with similar purpose by other Alternative features are replaced.That is, unless specifically stated, each feature is an example in a series of equivalent or similar characteristics ?.
Such as Fig. 1, the complicated radar overall pulse number production method of most prepulse specifically includes following procedure:
Step 1, first arrival pulse in radar signal pulse sequence is defined as the radar signal most prepulse, sought Look for the radar signal reached at first in simulated scenario most prepulse;
Preferably, the detailed process of the step 1 are as follows: step 11, by first arrival in radar signal pulse sequence Pulse is defined as the most prepulse of the radar signal, before describing word (PDW) parameter of the most prepulse includes most prepulse Along arrival time TOAi, carrier frequency RFi, pulse repetition period PRIi, pulse width PWi, impulse amplitude PAi, wherein i=0, 1 ..., ∞ is the number of radar signal;Step 12, the forward position of all radar signals most prepulse reaches in calculating simulation scene Time TOAi, unit is μ s, according to formulaSeek the smallest forward position arrival time TOAj, single Position is μ s (j ∈ { 0,1 ..., ∞ }, j are all corresponding radar signal numbers of the most prepulse reached at first searched out), Corresponding radar signal j is the radar signal most prepulse reached at first.
Step 2, describing word (PDW) parameter of radar signal most prepulse will be reached at first (when most prepulse forward position reaches Between TOAj, carrier frequency RFj, pulse width PWj, impulse amplitude PAj) be saved in interlaced pulse list to be output, it calculates and generates TOAjInterlaced pulse before moment.And this can be rejected from corresponding radar signal pulse sequence and reach radar signal most at first Prepulse.
Step 3, the forward position arrival time of radar signal most prepulse is updated;
Preferably, the detailed process of the step 3 are as follows: step 31, according toWherein, k is current PRF number, when k ∈ { 0,1 ..., ∞ }, k=0 pair Answer the most prepulse of radar signal j;TOAJ, 0The forward position arrival time of pulse, i.e. radar signal j may be reached for the 0th most The forward position arrival time TOA of prepulsej;TOAJ, k+1、TOAJ, kWhen respectively kth, the k+1 forward positions that may reach pulse reach Between;PRIJ, kFor the time interval between kth, the k+1 pulse that may be reached;Persistently iterative calculation radar signal j is next can The forward position arrival time TOA for the pulse that can be reachedJ, k+1It (is influenced by radar detection performance, is not all of radar generation The reachable radar detection intended recipient Antenna aperture of pulse);Step 32, the TOA of calculating is verifiedJ, k+1Whether iteration item is met Part, stopping criterion for iteration and radar detection performance are in relation to (it is assumed that only radar antenna main lobe and the irradiation of the first minor lobe main beam When to radar detection target, radar detection intended recipient antenna can just receive radar pulse), when radar detection performance is When tracking, stopping criterion for iteration is
TOAJ, k< TOAJ, k+1,
When radar detection performance is that circle is swept, stopping criterion for iteration is
When radar detection performance is fan sweeping, stopping criterion for iteration is
Or
Wherein, TjFor radar antenna scan period, W corresponding to radar signal jjIt is wide for wave beam corresponding to radar signal j Spend (main lobe and the first minor lobe width), aJ, 1For fan sweeping start angle, a corresponding to radar signal jJ, 2It is right for radar signal j The fan sweeping termination point answered works as TOA until meeting stopping criterion for iterationJ, k+1When meeting any of the above stopping criterion for iteration, TOAJ, k+1As acquire the forward position arrival time TOA of updated radar signal most prepulsej, obtain updated radar signal The forward position arrival time of most prepulse.
Step 4, for Radar Signal Transmission delay time, the forward position arrival time of radar signal most prepulse is corrected;
Since as radar in simulated scenario and the relative distance of radar detection target can change, Radar Signal Transmission Delay time tdIt will affect the forward position arrival time TOA of radar signal most prepulsej, it is preferable that the detailed process of the step 4 Are as follows: calculate Radar Signal Transmission delay time td=S/c × 103, S is the distance between radar and radar detection target, and unit is km;C is the light velocity, and value is 3.0 × 108m/s;The forward position arrival time of radar signal most prepulse is added into propagation delay time Between, obtain the forward position arrival time of revised radar signal most prepulse.
Step 5, the PDW parameter of radar signal most prepulse is updated;
Since the relative distance of the switching of radar working condition, radar and radar detection target in simulated scenario changes and answers Miscellaneous radar effect of signals, TOAjMoment reaches the signal parameter of the radar signal j of radar detection intended recipient Antenna aperture (the PDW parameter including most prepulse) will Development pattern variation, processing need to be updated to it.Preferably, the step 5 In, the PDW parameter of the update includes carrier frequency RFj, pulse repetition period PRIj, pulse width PWj, impulse amplitude PAj, described The renewal process that frequency carries is RFj'=RFj+ Δ RF × Rand (- 1,1), the renewal process of the pulse repetition period are PRIj'= PRIj+ Δ PRI × Rand (- 1,1), the pulse width PWjConstant, the renewal process of the impulse amplitude is
Wherein, TOA 'j, RFj′、PRIj', PWj′、PAj' be respectively updated radar signal j most prepulse forward position Arrival time, carrier frequency, pulse repetition period, pulse width, impulse amplitude, unit are respectively μ s, MHz, μ s, dBm;RFj、PRIj, PWj、PAjThe carrier frequency of radar signal j before respectively updating, pulse repetition period, pulse width, impulse amplitude, Rand (- 1,1) Indicate the random number generated in [- 1,1] range, PattenFor radar signal, signal power decays in free space transmission, and S is The distance between radar and radar detection target;Y (x) indicates radar directional pattern data, x ∈ [- 180 °, 180 °].
Step 6, the process of step 1-5 can realize that the calculating of single pulse generates, and repeat step 1~step 5, can be completed Complicated radar overall pulse is digitally generated.
For the validity for verifying most prepulse method algorithm, construction contains three radars (signal caused by three radars point Do not correspond to radar signal 1, radar signal 2, radar signal 3, three radars are switched on simultaneously when experiment) and a detection target mould Quasi- scene, wherein radar with and detection target it is opposing stationary, the relevant parameters such as radar, detection target describe in detail in simulated scenario It is shown in Table 1 (radar signal 2 and radar signal 3 be complicated radar signal), and by most prepulse method algorithm proposed by the present invention The overall pulse of arrival radar detection intended recipient Antenna aperture applied to the simulated scenario is digitally generated.
The relevant parameters such as radar describe in 1 simulated scenario of table
Table 2 is radar signal 1, the radar signal 2, radar being calculated using most prepulse method algorithm proposed by the present invention The overall pulse list of the arrival radar detection intended recipient Antenna aperture of signal 3.
The most prepulse method algorithm dynamic of table 2 calculates the interlaced pulse parameter list generated
Observation table 2 is it is recognized that while three radars are switched on simultaneously, but due to considering electromagnetic wave space propagation delay time to arteries and veins The influence of arrival time is rushed, three radar signals do not reach radar detection intended recipient Antenna aperture simultaneously.It is reached with pulse Time is abscissa, and impulse amplitude is ordinate, and draw to corresponding data in table 2 by Matlab can be observed, in arteries and veins Rushing arrival time is that 1s and 3s nearby has apparent cycle peak to occur (corresponding to main lobe and being irradiated to radar detection intended recipient antenna Mouthful face), and the period sweeps that the period is consistent with preset circle in table 1, so the overall pulse data of generation embody antenna scanning state And parameter.Therefore, the overall pulse data pulse that most prepulse method algorithm generates more meets reality, and fidelity is higher.
To sum up, most prepulse method proposed by the present invention is shown by core algorithm research, effect analysis and case verification Comprehensively consider whether radar antenna scanning generates pulse and the influence of impulse amplitude size, electromagnetic wave space propagation delay time Influence to pulse arrival time has the characteristics that scalability is strong, arithmetic speed is fast, simulation fidelity is high.
The invention is not limited to specific embodiments above-mentioned.The present invention, which expands to, any in the present specification to be disclosed New feature or any new combination, and disclose any new method or process the step of or any new combination.

Claims (6)

1. a kind of complicated radar overall pulse number production method based on most prepulse, which is characterized in that specifically include with Lower process: step 1, first arrival pulse in radar signal pulse sequence is defined as the radar signal most prepulse, is sought Look for the radar signal reached at first in simulated scenario most prepulse;Step 2, the description of radar signal most prepulse will be reached at first Word parameter is saved in interlaced pulse list to be output, is calculated and is generated interlaced pulse;Step 3, the most preceding arteries and veins of radar signal is updated The forward position arrival time of punching;Step 4, for Radar Signal Transmission delay time, the forward position for correcting radar signal most prepulse is arrived Up to the time;Step 5, the PDW parameter of radar signal most prepulse is updated;Step 6, it dynamically has been calculated and helps pulse digit generation.
2. the complicated radar overall pulse number production method based on most prepulse, feature exist as described in claim 1 In the detailed process of the step 1 are as follows: step 11, first arrival pulse in radar signal pulse sequence is defined as this The most prepulse of radar signal, the describing word parameter of the most prepulse include the forward position arrival time TOA of most prepulsei, carry Frequency RFi, pulse repetition period PRIi, pulse width PWi, impulse amplitude PAi, wherein i=0,1 ..., ∞ are radar signals Number;Step 12, in calculating simulation scene all radar signals most prepulse forward position arrival time TOAi, before asking the smallest Along arrival time TOAj(j ∈ { 0,1 ..., ∞ }), corresponding radar signal j are the radar signal most prepulse reached at first.
3. the complicated radar overall pulse number production method based on most prepulse, feature exist as claimed in claim 2 In, in the step 2, the forward position arrival time TOA of radar signal j most prepulsei, carrier frequency RFi, pulse repetition period PRIi、 Pulse width PWi, impulse amplitude PAiIt is saved among interlaced pulse list to be output, completes TOAjAll friendships before moment Wrong pulse, which calculates, to be generated.
4. the complicated radar overall pulse number production method based on most prepulse, feature exist as claimed in claim 3 In the detailed process of the step 3 are as follows: step 31, according toWherein, k is to work as Prepulse number, when k ∈ { 0,1 ..., ∞ }, k=0, correspond to the most prepulse of radar signal j;TOAJ, 0It may be reached for the 0th The forward position arrival time of pulse, i.e. the forward position arrival time TOA of the most prepulse of radar signal jj;TOAJ, k+1、TOAJ, kRespectively Kth, k+1 may reach the forward position arrival time of pulse;PRIJ, kFor the time between kth, the k+1 pulse that may be reached Interval;The persistently forward position arrival time TOA of the next possible pulse reached of iterative calculation radar signal jJ, k+1;Step 32, it tests Demonstrate,prove the TOA calculatedJ, k+1Whether iterated conditional is met, when radar detection performance is tracking, stopping criterion for iteration is
TOAJ, k< TOAJ, k+1,
When radar detection performance is that circle is swept, stopping criterion for iteration is
When radar detection performance is fan sweeping, stopping criterion for iteration is
Or
Wherein, TjFor radar antenna scan period, W corresponding to radar signal jjFor beam angle corresponding to radar signal j, aJ, 1For fan sweeping start angle, a corresponding to radar signal jJ, 2For fan sweeping termination point corresponding to radar signal j, until full Sufficient stopping criterion for iteration obtains the forward position arrival time of updated radar signal most prepulse.
5. the complicated radar overall pulse number production method based on most prepulse, feature exist as claimed in claim 4 In the detailed process of the step 4 are as follows: calculate Radar Signal Transmission delay time td=S/c × 103, S is that radar and radar are visited The distance between target is surveyed, c is the light velocity, and the forward position arrival time of radar signal most prepulse is added the propagation delay time, is obtained Take the forward position arrival time of revised radar signal most prepulse.
6. the complicated radar overall pulse number production method based on most prepulse, feature exist as claimed in claim 5 In in the step 5, the PDW parameter of the update includes carrier frequency RFj, pulse repetition period PRIj, pulse width PWj, pulse Amplitude PAj, the renewal process that the frequency carries is RFj'=RFj+ Δ RF × Rand (- 1,1), the update of the pulse repetition period Process is PRIj'=PRIj+ Δ PRI × Rand (- 1,1), the pulse width PWjIt is constant, the renewal process of the impulse amplitude For
Wherein, TOA 'j, RFj′、PRIj', PWj′、PAjThe forward position of ' respectively most the prepulse of updated radar signal j reaches Time, carrier frequency, pulse repetition period, pulse width, impulse amplitude, RFj、PRIj, PWj、PAjRadar letter before respectively updating The carrier frequency of number j, pulse repetition period, pulse width, impulse amplitude, Rand (- 1,1) indicate to generate in [- 1,1] range with Machine number, PattenFor radar signal in free space transmission signal power decay, S between radar and radar detection target away from From;Y (x) indicates radar directional pattern data, x ∈ [- 180 °, 180 °].
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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111654264A (en) * 2020-05-27 2020-09-11 桂林长海发展有限责任公司 Method and system for generating signal pulse sequence by signal data simulator

Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1432244A (en) * 1972-04-25 1976-04-14 Hollandse Signaalapparaten Bv Pulse radar apparatus
US4257108A (en) * 1977-12-27 1981-03-17 U.S. Philips Corporation Pulse generator
EP0452023A2 (en) * 1990-04-12 1991-10-16 Raytheon Company Method and apparatus for pulse sorting
CN1985187A (en) * 2004-07-16 2007-06-20 富士通天株式会社 Monopulse radar apparatus and antenna switch
CN104166136A (en) * 2014-07-11 2014-11-26 河海大学 Interference subspace tracking-based high-efficiency self-adaptive monopulse angle measurement method
CN104297730A (en) * 2014-10-17 2015-01-21 中国电子科技集团公司第二十九研究所 Method for obtaining radar clutter image
TW201510550A (en) * 2013-09-13 2015-03-16 Univ Nat Chiao Tung Comparator of mono-pulse radar and signal generation method thereof
US20170074973A1 (en) * 2015-09-10 2017-03-16 Herbert U. Fluhler Coherent integration of fill pulses in pulse doppler type sensors
CN107561499A (en) * 2017-07-27 2018-01-09 中国船舶重工集团公司第七二四研究所 A kind of how irregular signal sorting method of complexity based on EDW fusions

Patent Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1432244A (en) * 1972-04-25 1976-04-14 Hollandse Signaalapparaten Bv Pulse radar apparatus
US4257108A (en) * 1977-12-27 1981-03-17 U.S. Philips Corporation Pulse generator
EP0452023A2 (en) * 1990-04-12 1991-10-16 Raytheon Company Method and apparatus for pulse sorting
CN1985187A (en) * 2004-07-16 2007-06-20 富士通天株式会社 Monopulse radar apparatus and antenna switch
TW201510550A (en) * 2013-09-13 2015-03-16 Univ Nat Chiao Tung Comparator of mono-pulse radar and signal generation method thereof
CN104166136A (en) * 2014-07-11 2014-11-26 河海大学 Interference subspace tracking-based high-efficiency self-adaptive monopulse angle measurement method
CN104297730A (en) * 2014-10-17 2015-01-21 中国电子科技集团公司第二十九研究所 Method for obtaining radar clutter image
US20170074973A1 (en) * 2015-09-10 2017-03-16 Herbert U. Fluhler Coherent integration of fill pulses in pulse doppler type sensors
CN107561499A (en) * 2017-07-27 2018-01-09 中国船舶重工集团公司第七二四研究所 A kind of how irregular signal sorting method of complexity based on EDW fusions

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
张孝飞: ""脉冲发生器波形产生模块的设计与实现"", 《中国优秀博硕士学位论文全文数据库(硕士)信息科技辑》 *

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111654264A (en) * 2020-05-27 2020-09-11 桂林长海发展有限责任公司 Method and system for generating signal pulse sequence by signal data simulator
CN111654264B (en) * 2020-05-27 2023-04-28 桂林长海发展有限责任公司 Method and system for generating signal pulse sequence by signal data simulator

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