CN105759261B - A kind of automatic slow-down device with identification function - Google Patents
A kind of automatic slow-down device with identification function Download PDFInfo
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- CN105759261B CN105759261B CN201610089063.8A CN201610089063A CN105759261B CN 105759261 B CN105759261 B CN 105759261B CN 201610089063 A CN201610089063 A CN 201610089063A CN 105759261 B CN105759261 B CN 105759261B
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
- G01S13/00—Systems using the reflection or reradiation of radio waves, e.g. radar systems; Analogous systems using reflection or reradiation of waves whose nature or wavelength is irrelevant or unspecified
- G01S13/88—Radar or analogous systems specially adapted for specific applications
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
- G01S13/00—Systems using the reflection or reradiation of radio waves, e.g. radar systems; Analogous systems using reflection or reradiation of waves whose nature or wavelength is irrelevant or unspecified
- G01S13/88—Radar or analogous systems specially adapted for specific applications
- G01S13/93—Radar or analogous systems specially adapted for specific applications for anti-collision purposes
- G01S13/931—Radar or analogous systems specially adapted for specific applications for anti-collision purposes of land vehicles
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- 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
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
- G01S13/00—Systems using the reflection or reradiation of radio waves, e.g. radar systems; Analogous systems using reflection or reradiation of waves whose nature or wavelength is irrelevant or unspecified
- G01S13/88—Radar or analogous systems specially adapted for specific applications
- G01S13/93—Radar or analogous systems specially adapted for specific applications for anti-collision purposes
- G01S13/931—Radar or analogous systems specially adapted for specific applications for anti-collision purposes of land vehicles
- G01S2013/9321—Velocity regulation, e.g. cruise control
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- Radar, Positioning & Navigation (AREA)
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- Computer Networks & Wireless Communication (AREA)
- General Physics & Mathematics (AREA)
- Electromagnetism (AREA)
- Radar Systems Or Details Thereof (AREA)
Abstract
The invention discloses a kind of automatic slow-down device with identification function, including deceleration device and the millimetre-wave radar three-dimensional environment sensory perceptual system on deceleration device；Millimetre-wave radar three-dimensional environment sensory perceptual system includes millimetre-wave radar, rotation mechanism, control unit and data processing unit；Rotation mechanism includes the first rotary shaft, rotating disk and the second rotary shaft.This deceleration device is simple and practical, can realize that front is scanned without dead angle and cover, and has the advantages that control is accurate, setting accuracy is high, real-time is good.
Description
Technical field
The present invention relates to vehicle deceleration field, and in particular to a kind of automatic slow-down device with identification function.
Background technology
Broad street has driven urban development, is provided for the trip of people conveniently, with the development of science and technology, traffic intelligence
The concept of energyization is suggested, and increasing vehicle is mounted with automatic slow-down device.
The major function of intelligent environment sensory perceptual system is to obtain vehicle and environmental information, specially vehicle by sensor
Pose and state information acquisition, structuring highway in the lane line and recognition and tracking on lane side edge, traffic sign and traffic
The recognition and tracking of signal, motor vehicle environment barrier recognition and tracking (including dynamic and static-obstacle thing, as pedestrian,
Vehicle etc.) and vehicle running surface traffic analysis etc..
Deceleration device, intelligent environment sensory perceptual system is set to be to improve the combination properties such as its safety, multifunction thereon
Inevitable development trend at present.But present context aware systems often exist perceive dimension deficiency, computational accuracy it is not high,
The problems such as real-time is not strong.
The content of the invention
In view of the above-mentioned problems, the present invention provides a kind of automatic slow-down device with identification function.
The purpose of the present invention is realized using following technical scheme：
A kind of automatic slow-down device with identification function, including deceleration device and the millimeter wave on deceleration device
Radar three-dimensional context aware systems；Millimetre-wave radar three-dimensional environment sensory perceptual system includes millimetre-wave radar, rotation mechanism, control
Unit and data processing unit processed；Rotation mechanism includes the first rotary shaft, rotating disk and the second rotary shaft, the first rotary shaft
Arrange vertically and affixed with the center of rotating disk, first rotary shaft is rotated by the first driving stepper motor；By second step
Second rotation axis horizontal of stepper motor driving rotation is sleeved in bearing block, and the bearing block passes through 2 supports arranged vertically
Axle is affixed on the rotating pan；The midpoint of second rotary shaft is provided with connecting portion, and the connecting portion is perpendicular to the second rotation
Axle and it is integrally formed with the second rotary shaft, millimetre-wave radar is vertical with connecting portion affixed；The millimetre-wave radar itself is intrinsic
The plane of scanning motion is perpendicular to plane where rotating disk, and scanning range angle is ± 30 °；The rotating disk is in the side of arrangement support shaft
There is otch, the straight line parallel where otch is in the straight line where the second rotary shaft, and any support shaft and straight line where otch
Distance is less than 50mm；First stepper motor and the second stepper motor are controlled by single-chip microcomputer, and single-chip microcomputer is used to receive
Control command, and control command is converted into control signal and is sent to motor, while walked according to the initial position of device and two
The goniometer that stepper motor turns over calculates the current location of rotation mechanism, and the current position state of rotation mechanism is anti-
Feed data processing unit；The overall face forward under the drive of the first stepper motor of the rotation mechanism does 180 ° of level
Cycle back and forth movement, while millimetre-wave radar face forward under the drive of the second stepper motor do vertical 180 ° cycle it is past
Return motion；
Data processing unit includes data acquisition subelement, delay revise subelemen and coordinate output subelement；Data are adopted
Collection subelement receives its distance value ρ with target that millimetre-wave radar measurement obtains, while receives the vertical rotation of single-chip microcomputer transmission
Corner α and horizontal rotation angle beta, and itself scan angle theta of millimetre-wave radar；If millimetre-wave radar is to the reading of a certain target
(ρ, α, β, θ), and define：α=0 ° when radar is horizontal, when radar is horizontal top, α values are just thunder
It is negative up to α values when being horizontal lower section, β=0 ° when the second rotary shaft is vertical with direction immediately ahead of deceleration device, works as thunder
β is on the occasion of when radar is located at the left side of β=0 °, β is negative value during up to positioned at the right side of β=0 °；When millimetre-wave radar itself
θ=0 ° when scanning direction is vertical with plane where millimetre-wave radar, when itself scanning direction is located at the top of θ=0 °, θ is just
Value, when itself scanning direction is located at the lower section of θ=0 °, θ is negative value；
Preferably, delay revise subelemen includes range measurement correcting module, horizontal sweep correcting module and vertical scanning
Correcting module：Range measurement correcting module, the measured value for the value ρ that adjusts the distance, which be directed in detections of radar ripple two-way process, to be prolonged
Shi Xiaoying amendment, its modifying factor exported are：
When | α1+θ1| ＞ | α2+θ2| and | β1| ＞ | β2| when, above formula takes positive sign, otherwise takes negative sign；
Vertical scanning correcting module, imitated for be directed to being delayed in detections of radar ripple two-way process to vertical rotary angle α
The amendment answered, its modifying factor exportedWhen | α1| ＞ | α2| when, above formula takes positive sign, otherwise takes
Negative sign；
Horizontal sweep correcting module, for carrying out being directed in detections of radar ripple two-way process the effect that is delayed to rotating horizontally angle beta
The amendment answered, its modifying factor exportedWhen | β1| ＞ | β2| when, above formula takes positive sign, otherwise
Take negative sign；
Wherein m is the maximum detectable range of millimetre-wave radar, and ρ≤m；For reaction detection target and millimeter wave thunder
Influence of the distance to delay effect between reaching, target be then delayed closer to radar it is smaller, otherwise delay it is bigger；t1For to the target
The time that detections of radar ripple is sent, t2The time returned for detections of radar ripple；|t1-t2| represent detections of radar ripple and travel to and fro between mesh
Time needed between mark and radar；T1For the horizontal rotation cycle of millimetre-wave radar, T2For the vertical revolution of millimetre-wave radar
Phase；α1For t1When α values, α2For t2When α values；β1For t1When β value, β2For t2When β value；θ1For t1When θ values, θ2For t2When
θ values；T1=2s, T2=2.4s, the sampling interval of millimetre-wave radar is 2 °/s；
Coordinate exports subelement：The object space coordinate exported after the revise subelemen amendment that is delayed is：
Wherein,
Data processing unit also includes target RCS fluctuation characteristics measurement subelement, for the RCS sequence variations system to target
Number measures：
Complex target for being in optical region, it is assumed that be made up of N number of scattering center, then multi-scattering centers target
RCS is expressed as the function of azimuth of target：
Wherein, σiRepresent that i-th of scattering center RCS, α+θ represents target with respect to the azimuth of millimetre-wave radar, RiRepresent the
I scattering center is with respect to radar center distance；λ is the parameter being manually set；
Then RCS sequence variations coefficient is expressed as：Wherein σ (k) represents kth time detection
The RCS values of target, RCS serial means
This deceleration device has the beneficial effect that：New millimetre-wave radar three-dimensional environment sensory perceptual system is devised, so as to realize
180 ° of front horizontal and being scanned without dead angle for 180 ° of vertical direction cover, and economy and durability simple in construction, strong antijamming capability；Profit
Other parts are coordinated to realize Automatic Control function with step-by-step motor, it is easy to control accurate；For new-type rotating radar system
The characteristics of system and delay effect devise range measurement correcting module, horizontal sweep correcting module, vertical scanning correcting module
Deng correcting module so that the coordinate setting function of radar is more accurate, and real-time is stronger；Give accurate coordinate calculating side
Method, provided the foundation to automatically control with control errors；For the Novel rotary mechanical device, employ new RCS and play volt
Property measurement apparatus so that the measurement of the RCS coefficient of variation is more accurate, more favourable to target identification；The parts such as rotating disk, rotary shaft
Size can flexibly choose as the case may be, the applicability for various different size of deceleration devices provides condition；With milli
Metre wave radar substitutes traditional light wave radar, and decay when being propagated using atmospheric window is small, is influenceed by natural light and infrared source
It is small, target can effectively be identified under atrocious weather situation, provide reliable guarantee for safety traffic, there is high-resolution
The superiority such as power, high accuracy, miniature antenna bore.
Brief description of the drawings
Using accompanying drawing, the invention will be further described, but the embodiment in accompanying drawing does not form any limit to the present invention
System, for one of ordinary skill in the art, on the premise of not paying creative work, can also be obtained according to the following drawings
Other accompanying drawings.
Fig. 1 is a kind of structured flowchart of the automatic slow-down device with identification function；
Fig. 2 is the structural representation of rotation mechanism；
Fig. 3 is millimetre-wave radar itself scanning schematic diagram；
Schematic diagram when Fig. 4 is detections of radar target；
Fig. 5 is the structured flowchart of data processing unit.
Reference：Millimetre-wave radar -1；Rotating disk -2；First rotary shaft -3；Second rotary shaft -4；Bearing block -5；Branch
Support axle -6；Connecting portion -7；First stepper motor -8；Second stepper motor -9；Rotation mechanism -10；Control unit -11；Number
According to processing unit -12；Data acquisition subelement 13；Be delayed revise subelemen -14；Coordinate exports subelement -15；Otch -16；Mesh
Mark -17；Front -18.
Embodiment
The invention will be further described with the following Examples.
Embodiment 1：
A kind of automatic slow-down device with identification function as Figure 1-4, including deceleration device and installed in deceleration
Millimetre-wave radar three-dimensional environment sensory perceptual system on device；Millimetre-wave radar three-dimensional environment sensory perceptual system include millimetre-wave radar 1,
Rotation mechanism 10, control unit 11 and data processing unit 12；Rotation mechanism bag 10 includes the first rotary shaft 3, rotation
The rotary shaft 4 of disk 2 and second, the first rotary shaft 3 arrangement and affixed with the center of rotating disk 2 vertically, first rotary shaft 3 passes through
The driving rotation of first stepper motor 8；The horizontal set of the second rotary shaft 4 of rotation is driven in bearing block 5 by the second stepper motor 9
Interior, the bearing block 5 is fixed in rotating disk 2 by 2 support shafts arranged vertically 6；The midpoint of second rotary shaft 4
Connecting portion 7 is provided with, the connecting portion 7 is integrally formed perpendicular to the second rotary shaft 4 and with the second rotary shaft 4, millimetre-wave radar 1
It is vertical with connecting portion 7 affixed；Itself intrinsic plane of scanning motion of the millimetre-wave radar 1 is swept perpendicular to the place plane of rotating disk 2
Range angle is retouched as ± 30 °；The rotating disk 2 has an otch 16 in the side of arrangement support shaft 6, the straight line parallel where otch 16 in
Straight line where second rotary shaft 4, and any support shaft 6 and the distance of the place straight line of otch 16 are less than 50mm；The first step
The stepper motor 9 of stepper motor 8 and second is controlled by single-chip microcomputer, and single-chip microcomputer is used to receive control command, and by control command
It is converted into control signal and is sent to motor, while the goniometer turned over according to the initial position of device and two stepper motors calculates
The current location of rotation mechanism, and the current position state of rotation mechanism 10 is fed back into data processing unit 12；
The cycle that the overall face forward 18 under the drive of the first stepper motor 8 of the rotation mechanism 10 does 180 ° of level comes and goes fortune
It is dynamic, while the face forward 20 under the drive of the second stepper motor 9 of millimetre-wave radar 1 does vertical 180 ° of cycle back and forth movement；
As shown in figure 5, data processing unit 12 is defeated including data acquisition subelement 13, delay revise subelemen 14 and coordinate
Go out subelement 15, data acquisition subelement 13 receives millimetre-wave radar 1 and measures its obtained distance value ρ with target, connects simultaneously
The vertical rotary angle α and rotate horizontally angle beta that single-chip microcomputer sends, and millimetre-wave radar 1 scan angle theta of itself are received, so as to obtain
The position of complete millimetre-wave radar data and the plane of scanning motion；As shown in figure 5, set a certain target 17 that millimetre-wave radar 1 measures
Reading be (ρ, α, β, θ), and define：α=0 ° when millimetre-wave radar 1 is horizontal, when millimetre-wave radar 1 is in water
α values is just, α values are negative when millimetre-wave radar 1 is horizontal lower section when prosposition puts top；When the second rotary shaft 4 is with slowing down
β=0 ° when direction is vertical immediately ahead of device, when millimetre-wave radar 1 is located at the right side of β=0 °, β is on the occasion of when millimetre-wave radar 1
β is negative value during positioned at the left side of β=0 °；When itself scanning direction of millimetre-wave radar 1 is vertical with the place plane of millimetre-wave radar 1
When θ=0 °, when itself scanning direction is located at the top of θ=0 ° θ be on the occasion of when itself scanning direction is located at the lower section of θ=0 °
When θ be negative value.The anglec of rotation β of the first rotary shaft 3 is the anglec of rotation of millimetre-wave radar 1 in the horizontal direction as shown in Figure 3.
Preferably, delay effect refers to, because the present apparatus is using the technical scheme of three dimensionality dual rotary, therefore in thunder
Up to detection ripple during be issued to return, the position of radar has occurred that certain skew, although this period is very short,
But when rotary speed is higher, the error of this part is still very important, this is that the present apparatus fills with the detection of other fixed radars
Put different place, it is therefore necessary to introduce special delay correction factor.Delay revise subelemen 14 is repaiied including range measurement
Positive module, horizontal sweep correcting module and vertical scanning correcting module：Range measurement correcting module, the survey for the value ρ that adjusts the distance
Value be directed to the amendment of delay effect in detections of radar ripple two-way process, and its modifying factor exported is：
When | α1+θ1| ＞ | α2+θ2| and | β1| ＞ | β2| when, illustrate that the rotation of device is towards the direction motion of target point
, the actual value now measured is less than normal, therefore above formula uses positive sign, now λρ＞ 1, otherwise use negative sign, now λρ＜ 1；Meanwhile
Due to t1-t2It is the value of a very little, therefore the specific correction value of this correcting module depends entirely on the swing circle T of motor, rotation
Turn faster T it is smaller, then correction factor with 1 poor absolute value it is bigger, it is on the contrary then smaller.
Vertical scanning correcting module, imitated for be directed to being delayed in detections of radar ripple two-way process to vertical rotary angle α
The amendment answered, its modifying factor exportedWhen | α1| ＞ | α2| when, above formula takes positive sign, otherwise takes
Negative sign；
Horizontal sweep correcting module, for carrying out being directed in detections of radar ripple two-way process the effect that is delayed to rotating horizontally angle beta
The amendment answered, its modifying factor exportedWhen | β1| ＞ | β2| when, above formula takes positive sign, otherwise
Take negative sign；
Wherein m is the maximum detectable range of millimetre-wave radar 1, and ρ≤m；For reaction detection target 17 and millimeter wave
Influence of the distance to delay effect between radar 1, target 17 be then delayed closer to millimetre-wave radar 1 it is smaller, otherwise delay it is bigger；
t1For the time sent to the detections of radar ripple of target 17, t2The time returned for detections of radar ripple, then | t1-t2| represent thunder
Time needed for being travelled to and fro between up to detection ripple between target 17 and millimetre-wave radar 1；t1For the horizontal rotation week of millimetre-wave radar 1
Phase, t2For the vertical swing circle of millimetre-wave radar 1；α1For t1When α values, α2For t2When α values；β1For t1When β value, β2For
t2When β value；θ1For t1When θ values, θ2For t2When θ values；T1=2s, T2=2.4s, sampling interval of millimetre-wave radar for 2 °/
s。
Coordinate exports subelement 15：The object space coordinate exported after the revise subelemen amendment that is delayed is：
Wherein,
Data processing unit also includes target RCS fluctuation characteristics measurement subelement, for the RCS sequence variations system to target
Number measures, and radar cross section (RCS) value characterizes the ability of reception antenna direction target echo, by measuring target
RCS fluctuation characteristics, which can contrast, determines different target types.
Complex target for being in optical region, it is assumed that it is made up of N number of scattering center, can according to radar scattering theory
Know, radar return can regard the echo Vector modulation of multi-scattering centers as, due to sight of each scattering center with respect to radar
Angle is different so that in Vector modulation, respective relative phase changes the fluctuations for causing echo signal amplitude, RCS at random
Value, which follows, also there are fluctuations.Therefore radar target RCS changes very sensitive, target RCS time sequences to the attitude angle of target
Row are substantially variable quantities of the RCS with azimuth of target, are a relief volumes, then the RCS of multi-scattering centers target is expressed as mesh
Mark azimuthal function：
Wherein, σiRepresent that i-th of scattering center RCS, α+θ represents target with respect to the azimuth of millimetre-wave radar, RiRepresent the
I scattering center is with respect to radar center distance；λ is the parameter being manually set；
Then RCS sequence variations coefficient is expressed as：Wherein σ (k) represents kth time detection
The RCS values of target, RCS serial meansSequence variations coefficient and azimuth are inputted as characteristic parameter
Target identification system is to complete the identification to target.
In this embodiment, new millimetre-wave radar three-dimensional environment sensory perceptual system is devised for deceleration device, so as to realize
180 ° of front horizontal and being scanned without dead angle for 180 ° of vertical direction cover, and economy and durability simple in construction, strong antijamming capability；Profit
Other parts are coordinated to realize Automatic Control function with step-by-step motor, it is easy to control accurate；For new-type rotating radar system
The characteristics of system and delay effect devise range measurement correcting module, horizontal sweep correcting module, vertical scanning correcting module
Deng correcting module so that the coordinate setting function of radar is more accurate, sets T1=2s, T2=2.4s, between the sampling of millimetre-wave radar
2 °/s is divided into, is realizing that measurement error is less than 1%, and measurement delay rate is less than 0.5%, and real-time while detection without dead angle
It is stronger；Accurate Coordinate calculation method is given, is provided the foundation to automatically control with control errors；Made a connection for the novel rotary
Tool device, employ new RCS fluctuation characteristic measurement apparatus so that the measurement of the RCS coefficient of variation is more accurate, to target identification
It is more favourable；The size of the parts such as rotating disk, rotary shaft can flexibly be chosen as the case may be, for the various different size of dresses that slow down
The applicability put provides condition；Substitute traditional light wave radar, decay when being propagated using atmospheric window with millimetre-wave radar
It is small, influenceed by natural light and infrared source small, target can effectively be identified under atrocious weather situation, be security row
Offer reliable guarantee is provided, there is the superiority such as high resolution, high accuracy, miniature antenna bore, achieve unexpected effect.
Embodiment 2：
A kind of automatic slow-down device with identification function as Figure 1-4, including deceleration device and installed in deceleration
Millimetre-wave radar three-dimensional environment sensory perceptual system on device；Millimetre-wave radar three-dimensional environment sensory perceptual system include millimetre-wave radar 1,
Rotation mechanism 10, control unit 11 and data processing unit 12；Rotation mechanism bag 10 includes the first rotary shaft 3, rotation
The rotary shaft 4 of disk 2 and second, the first rotary shaft 3 arrangement and affixed with the center of rotating disk 2 vertically, first rotary shaft 3 passes through
The driving rotation of first stepper motor 8；The horizontal set of the second rotary shaft 4 of rotation is driven in bearing block 5 by the second stepper motor 9
Interior, the bearing block 5 is fixed in rotating disk 2 by 2 support shafts arranged vertically 6；The midpoint of second rotary shaft 4
Connecting portion 7 is provided with, the connecting portion 7 is integrally formed perpendicular to the second rotary shaft 4 and with the second rotary shaft 4, millimetre-wave radar 1
It is vertical with connecting portion 7 affixed；Itself intrinsic plane of scanning motion of the millimetre-wave radar 1 is swept perpendicular to the place plane of rotating disk 2
Range angle is retouched as ± 30 °；The rotating disk 2 has an otch 16 in the side of arrangement support shaft 6, the straight line parallel where otch 16 in
Straight line where second rotary shaft 4, and any support shaft 6 and the distance of the place straight line of otch 16 are less than 50mm；The first step
The stepper motor 9 of stepper motor 8 and second is controlled by single-chip microcomputer, and single-chip microcomputer is used to receive control command, and by control command
It is converted into control signal and is sent to motor, while the goniometer turned over according to the initial position of device and two stepper motors calculates
The current location of rotation mechanism, and the current position state of rotation mechanism 10 is fed back into data processing unit 12；
The cycle that the overall face forward 18 under the drive of the first stepper motor 8 of the rotation mechanism 10 does 180 ° of level comes and goes fortune
It is dynamic, while the face forward 20 under the drive of the second stepper motor 9 of millimetre-wave radar 1 does vertical 180 ° of cycle back and forth movement；
As shown in figure 5, data processing unit 12 is defeated including data acquisition subelement 13, delay revise subelemen 14 and coordinate
Go out subelement 15, data acquisition subelement 13 receives millimetre-wave radar 1 and measures its obtained distance value ρ with target, connects simultaneously
The vertical rotary angle α and rotate horizontally angle beta that single-chip microcomputer sends, and millimetre-wave radar 1 scan angle theta of itself are received, so as to obtain
The position of complete millimetre-wave radar data and the plane of scanning motion；As shown in figure 5, set a certain target 17 that millimetre-wave radar 1 measures
Reading be (ρ, α, β, θ), and define：α=0 ° when millimetre-wave radar 1 is horizontal, when millimetre-wave radar 1 is in water
α values is just, α values are negative when millimetre-wave radar 1 is horizontal lower section when prosposition puts top；When the second rotary shaft 4 is with slowing down
β=0 ° when direction is vertical immediately ahead of device, when millimetre-wave radar 1 is located at the right side of β=0 °, β is on the occasion of when millimetre-wave radar 1
β is negative value during positioned at the left side of β=0 °；When itself scanning direction of millimetre-wave radar 1 is vertical with the place plane of millimetre-wave radar 1
When θ=0 °, when itself scanning direction is located at the top of θ=0 ° θ be on the occasion of when itself scanning direction is located at the lower section of θ=0 °
When θ be negative value.The anglec of rotation β of the first rotary shaft 3 is the anglec of rotation of millimetre-wave radar 1 in the horizontal direction as shown in Figure 3.
Preferably, delay effect refers to, because the present apparatus is using the technical scheme of three dimensionality dual rotary, therefore in thunder
Up to detection ripple during be issued to return, the position of radar has occurred that certain skew, although this period is very short,
But when rotary speed is higher, the error of this part is still very important, this is that the present apparatus fills with the detection of other fixed radars
Put different place, it is therefore necessary to introduce special delay correction factor.Delay revise subelemen 14 is repaiied including range measurement
Positive module, horizontal sweep correcting module and vertical scanning correcting module：Range measurement correcting module, the survey for the value ρ that adjusts the distance
Value be directed to the amendment of delay effect in detections of radar ripple two-way process, and its modifying factor exported is：
When | α1+θ1| ＞ | α2+θ2| and | β1| ＞ | β2| when, illustrate that the rotation of device is towards the direction motion of target point
, the actual value now measured is less than normal, therefore above formula uses positive sign, now λρ＞ 1, otherwise use negative sign, now λρ＜ 1；Meanwhile
Due to t1-t2It is the value of a very little, therefore the specific correction value of this correcting module depends entirely on the swing circle T of motor, rotation
Turn faster T it is smaller, then correction factor with 1 poor absolute value it is bigger, it is on the contrary then smaller.
Vertical scanning correcting module, imitated for be directed to being delayed in detections of radar ripple two-way process to vertical rotary angle α
The amendment answered, its modifying factor exportedWhen | α1| ＞ | α2| when, above formula takes positive sign, otherwise takes
Negative sign；
Horizontal sweep correcting module, for carrying out being directed in detections of radar ripple two-way process the effect that is delayed to rotating horizontally angle beta
The amendment answered, its modifying factor exportedWhen | β1| ＞ | β2| when, above formula takes positive sign, otherwise
Take negative sign；
Wherein m is the maximum detectable range of millimetre-wave radar 1, and ρ≤m；For reaction detection target 17 and millimeter wave
Influence of the distance to delay effect between radar 1, target 17 be then delayed closer to millimetre-wave radar 1 it is smaller, otherwise delay it is bigger；
t1For the time sent to the detections of radar ripple of target 17, t2The time returned for detections of radar ripple, then | t1-t2| represent thunder
Time needed for being travelled to and fro between up to detection ripple between target 17 and millimetre-wave radar 1；t1For the horizontal rotation week of millimetre-wave radar 1
Phase, t2For the vertical swing circle of millimetre-wave radar 1；α1For t1When α values, α2For t2When α values；β1For t1When β value, β2For
t2When β value；θ1For t1When θ values, θ2For t2When θ values；T1=2s, T2=2.4s, sampling interval of millimetre-wave radar for 2 °/
s。
Coordinate exports subelement 15：The object space coordinate exported after the revise subelemen amendment that is delayed is：
Wherein,
Data processing unit also includes target RCS fluctuation characteristics measurement subelement, for the RCS sequence variations system to target
Number measures, and radar cross section (RCS) value characterizes the ability of reception antenna direction target echo, by measuring target
RCS fluctuation characteristics, which can contrast, determines different target types.
Complex target for being in optical region, it is assumed that it is made up of N number of scattering center, can according to radar scattering theory
Know, radar return can regard the echo Vector modulation of multi-scattering centers as, due to sight of each scattering center with respect to radar
Angle is different so that in Vector modulation, respective relative phase changes the fluctuations for causing echo signal amplitude, RCS at random
Value, which follows, also there are fluctuations.Therefore radar target RCS changes very sensitive, target RCS time sequences to the attitude angle of target
Row are substantially variable quantities of the RCS with azimuth of target, are a relief volumes, then the RCS of multi-scattering centers target is expressed as mesh
Mark azimuthal function：
Wherein, σiRepresent that i-th of scattering center RCS, α+θ represents azimuth of the target with respect to millimetre-wave radar, Ri is represented
I-th of scattering center is with respect to radar center distance；λ is the parameter being manually set；
Then RCS sequence variations coefficient is expressed as：Wherein σ (k) represents kth time detection
The RCS values of target, RCS serial meansSequence variations coefficient and azimuth are inputted as characteristic parameter
Target identification system is to complete the identification to target.
In this embodiment, new millimetre-wave radar three-dimensional environment sensory perceptual system is devised for deceleration device, so as to realize
180 ° of front horizontal and being scanned without dead angle for 180 ° of vertical direction cover, and economy and durability simple in construction, strong antijamming capability；Profit
Other parts are coordinated to realize Automatic Control function with step-by-step motor, it is easy to control accurate；For new-type rotating radar system
The characteristics of system and delay effect devise range measurement correcting module, horizontal sweep correcting module, vertical scanning correcting module
Deng correcting module so that the coordinate setting function of radar is more accurate, sets T1=2.2s, T2=2.6s, the sampling of millimetre-wave radar
At intervals of 1.5 °/s, realizing that measurement error is less than 0.8% while detection without dead angle, measuring delay rate less than 0.4%, and
Real-time is stronger；Accurate Coordinate calculation method is given, is provided the foundation to automatically control with control errors；It is new for this
Rotation mechanism, employ new RCS fluctuation characteristic measurement apparatus so that the measurement of the RCS coefficient of variation is more accurate, to mesh
Mark is not more favourable；The size of the parts such as rotating disk, rotary shaft can flexibly be chosen as the case may be, be various different size of
The applicability of deceleration device provides condition；Substitute traditional light wave radar with millimetre-wave radar, when being propagated using atmospheric window
Decay it is small, influenceed by natural light and infrared source small, target can effectively be identified under atrocious weather situation, be
Safety traffic provides reliable guarantee, has the superiority such as high resolution, high accuracy, miniature antenna bore, achieves unexpected
Effect.
Embodiment 3：
A kind of automatic slow-down device with identification function as Figure 1-4, including deceleration device and installed in deceleration
Millimetre-wave radar three-dimensional environment sensory perceptual system on device；Millimetre-wave radar three-dimensional environment sensory perceptual system include millimetre-wave radar 1,
Rotation mechanism 10, control unit 11 and data processing unit 12；Rotation mechanism bag 10 includes the first rotary shaft 3, rotation
The rotary shaft 4 of disk 2 and second, the first rotary shaft 3 arrangement and affixed with the center of rotating disk 2 vertically, first rotary shaft 3 passes through
The driving rotation of first stepper motor 8；The horizontal set of the second rotary shaft 4 of rotation is driven in bearing block 5 by the second stepper motor 9
Interior, the bearing block 5 is fixed in rotating disk 2 by 2 support shafts arranged vertically 6；The midpoint of second rotary shaft 4
Connecting portion 7 is provided with, the connecting portion 7 is integrally formed perpendicular to the second rotary shaft 4 and with the second rotary shaft 4, millimetre-wave radar 1
It is vertical with connecting portion 7 affixed；Itself intrinsic plane of scanning motion of the millimetre-wave radar 1 is swept perpendicular to the place plane of rotating disk 2
Range angle is retouched as ± 30 °；The rotating disk 2 has an otch 16 in the side of arrangement support shaft 6, the straight line parallel where otch 16 in
Straight line where second rotary shaft 4, and any support shaft 6 and the distance of the place straight line of otch 16 are less than 50mm；The first step
The stepper motor 9 of stepper motor 8 and second is controlled by single-chip microcomputer, and single-chip microcomputer is used to receive control command, and by control command
It is converted into control signal and is sent to motor, while the goniometer turned over according to the initial position of device and two stepper motors calculates
The current location of rotation mechanism, and the current position state of rotation mechanism 10 is fed back into data processing unit 12；
The cycle that the overall face forward 18 under the drive of the first stepper motor 8 of the rotation mechanism 10 does 180 ° of level comes and goes fortune
It is dynamic, while the face forward 20 under the drive of the second stepper motor 9 of millimetre-wave radar 1 does vertical 180 ° of cycle back and forth movement；
As shown in figure 5, data processing unit 12 is defeated including data acquisition subelement 13, delay revise subelemen 14 and coordinate
Go out subelement 15, data acquisition subelement 13 receives millimetre-wave radar 1 and measures its obtained distance value ρ with target, connects simultaneously
The vertical rotary angle α and rotate horizontally angle beta that single-chip microcomputer sends, and millimetre-wave radar 1 scan angle theta of itself are received, so as to obtain
The position of complete millimetre-wave radar data and the plane of scanning motion；As shown in figure 5, set a certain target 17 that millimetre-wave radar 1 measures
Reading be (ρ, α, β, θ), and define：α=0 ° when millimetre-wave radar 1 is horizontal, when millimetre-wave radar 1 is in water
α values is just, α values are negative when millimetre-wave radar 1 is horizontal lower section when prosposition puts top；When the second rotary shaft 4 is with slowing down
β=0 ° when direction is vertical immediately ahead of device, when millimetre-wave radar 1 is located at the right side of β=0 °, β is on the occasion of when millimetre-wave radar 1
β is negative value during positioned at the left side of β=0 °；When itself scanning direction of millimetre-wave radar 1 is vertical with the place plane of millimetre-wave radar 1
When θ=0 °, when itself scanning direction is located at the top of θ=0 ° θ be on the occasion of when itself scanning direction is located at the lower section of θ=0 °
When θ be negative value.The anglec of rotation β of the first rotary shaft 3 is the anglec of rotation of millimetre-wave radar 1 in the horizontal direction as shown in Figure 3.
Preferably, delay effect refers to, because the present apparatus is using the technical scheme of three dimensionality dual rotary, therefore in thunder
Up to detection ripple during be issued to return, the position of radar has occurred that certain skew, although this period is very short,
But when rotary speed is higher, the error of this part is still very important, this is that the present apparatus fills with the detection of other fixed radars
Put different place, it is therefore necessary to introduce special delay correction factor.Delay revise subelemen 14 is repaiied including range measurement
Positive module, horizontal sweep correcting module and vertical scanning correcting module：Range measurement correcting module, the survey for the value ρ that adjusts the distance
Value be directed to the amendment of delay effect in detections of radar ripple two-way process, and its modifying factor exported is：
When | α1+θ1| ＞ | α2+θ2| and | β1| ＞ | β2| when, illustrate that the rotation of device is towards the direction motion of target point
, the actual value now measured is less than normal, therefore above formula uses positive sign, now λρ＞ 1, otherwise use negative sign, now λρ＜ 1；Meanwhile
Due to t1-t2It is the value of a very little, therefore the specific correction value of this correcting module depends entirely on the swing circle T of motor, rotation
Turn faster T it is smaller, then correction factor with 1 poor absolute value it is bigger, it is on the contrary then smaller.
Vertical scanning correcting module, imitated for be directed to being delayed in detections of radar ripple two-way process to vertical rotary angle α
The amendment answered, its modifying factor exportedWhen | α1| ＞ | α2| when, above formula takes positive sign, otherwise takes
Negative sign；
Horizontal sweep correcting module, for carrying out being directed in detections of radar ripple two-way process the effect that is delayed to rotating horizontally angle beta
The amendment answered, its modifying factor exportedWhen | β1| ＞ | β2| when, above formula takes positive sign, otherwise
Take negative sign；
Wherein m is the maximum detectable range of millimetre-wave radar 1, and ρ≤m；For reaction detection target 17 and millimeter wave
Influence of the distance to delay effect between radar 1, target 17 be then delayed closer to millimetre-wave radar 1 it is smaller, otherwise delay it is bigger；
t1For the time sent to the detections of radar ripple of target 17, t2The time returned for detections of radar ripple, then | t1-t2| represent thunder
Time needed for being travelled to and fro between up to detection ripple between target 17 and millimetre-wave radar 1；t1For the horizontal rotation week of millimetre-wave radar 1
Phase, t2For the vertical swing circle of millimetre-wave radar 1；α1For t1When α values, α2For t2When α values；β1For t1When β value, β2For
t2When β value；θ1For t1When θ values, θ2For t2When θ values；T1=2s, T2=2.4s, sampling interval of millimetre-wave radar for 2 °/
s。
Coordinate exports subelement 15：The object space coordinate exported after the revise subelemen amendment that is delayed is：
Wherein,
Data processing unit also includes target RCS fluctuation characteristics measurement subelement, for the RCS sequence variations system to target
Number measures, and radar cross section (RCS) value characterizes the ability of reception antenna direction target echo, by measuring target
RCS fluctuation characteristics, which can contrast, determines different target types.
Complex target for being in optical region, it is assumed that it is made up of N number of scattering center, can according to radar scattering theory
Know, radar return can regard the echo Vector modulation of multi-scattering centers as, due to sight of each scattering center with respect to radar
Angle is different so that in Vector modulation, respective relative phase changes the fluctuations for causing echo signal amplitude, RCS at random
Value, which follows, also there are fluctuations.Therefore radar target RCS changes very sensitive, target RCS time sequences to the attitude angle of target
Row are substantially variable quantities of the RCS with azimuth of target, are a relief volumes, then the RCS of multi-scattering centers target is expressed as mesh
Mark azimuthal function：
Wherein, σiRepresent that i-th of scattering center RCS, α+θ represents target with respect to the azimuth of millimetre-wave radar, RiRepresent the
I scattering center is with respect to radar center distance；λ is the parameter being manually set；
Then RCS sequence variations coefficient is expressed as：Wherein σ (k) represents kth time detection
The RCS values of target, RCS serial meansSequence variations coefficient and azimuth are inputted as characteristic parameter
Target identification system is to complete the identification to target.
In this embodiment, new millimetre-wave radar three-dimensional environment sensory perceptual system is devised for deceleration device, so as to realize
180 ° of front horizontal and being scanned without dead angle for 180 ° of vertical direction cover, and economy and durability simple in construction, strong antijamming capability；Profit
Other parts are coordinated to realize Automatic Control function with step-by-step motor, it is easy to control accurate；For new-type rotating radar system
The characteristics of system and delay effect devise range measurement correcting module, horizontal sweep correcting module, vertical scanning correcting module
Deng correcting module so that the coordinate setting function of radar is more accurate, sets T1=2.4s, T2=2.7s, the sampling of millimetre-wave radar
At intervals of 1.8 °/s, realizing that measurement error is less than 0.7% while detection without dead angle, measuring delay rate less than 0.4%, and
Real-time is stronger；Accurate Coordinate calculation method is given, is provided the foundation to automatically control with control errors；It is new for this
Rotation mechanism, employ new RCS fluctuation characteristic measurement apparatus so that the measurement of the RCS coefficient of variation is more accurate, to mesh
Mark is not more favourable；The size of the parts such as rotating disk, rotary shaft can flexibly be chosen as the case may be, be various different size of
The applicability of deceleration device provides condition；Substitute traditional light wave radar with millimetre-wave radar, when being propagated using atmospheric window
Decay it is small, influenceed by natural light and infrared source small, target can effectively be identified under atrocious weather situation, be
Safety traffic provides reliable guarantee, has the superiority such as high resolution, high accuracy, miniature antenna bore, achieves unexpected
Effect.
Embodiment 4：
A kind of automatic slow-down device with identification function as Figure 1-4, including deceleration device and installed in deceleration
Millimetre-wave radar three-dimensional environment sensory perceptual system on device；Millimetre-wave radar three-dimensional environment sensory perceptual system include millimetre-wave radar 1,
Rotation mechanism 10, control unit 11 and data processing unit 12；Rotation mechanism bag 10 includes the first rotary shaft 3, rotation
The rotary shaft 4 of disk 2 and second, the first rotary shaft 3 arrangement and affixed with the center of rotating disk 2 vertically, first rotary shaft 3 passes through
The driving rotation of first stepper motor 8；The horizontal set of the second rotary shaft 4 of rotation is driven in bearing block 5 by the second stepper motor 9
Interior, the bearing block 5 is fixed in rotating disk 2 by 2 support shafts arranged vertically 6；The midpoint of second rotary shaft 4
Connecting portion 7 is provided with, the connecting portion 7 is integrally formed perpendicular to the second rotary shaft 4 and with the second rotary shaft 4, millimetre-wave radar 1
It is vertical with connecting portion 7 affixed；Itself intrinsic plane of scanning motion of the millimetre-wave radar 1 is swept perpendicular to the place plane of rotating disk 2
Range angle is retouched as ± 30 °；The rotating disk 2 has an otch 16 in the side of arrangement support shaft 6, the straight line parallel where otch 16 in
Straight line where second rotary shaft 4, and any support shaft 6 and the distance of the place straight line of otch 16 are less than 50mm；The first step
The stepper motor 9 of stepper motor 8 and second is controlled by single-chip microcomputer, and single-chip microcomputer is used to receive control command, and by control command
It is converted into control signal and is sent to motor, while the goniometer turned over according to the initial position of device and two stepper motors calculates
The current location of rotation mechanism, and the current position state of rotation mechanism 10 is fed back into data processing unit 12；
The cycle that the overall face forward 18 under the drive of the first stepper motor 8 of the rotation mechanism 10 does 180 ° of level comes and goes fortune
It is dynamic, while the face forward 20 under the drive of the second stepper motor 9 of millimetre-wave radar 1 does vertical 180 ° of cycle back and forth movement；
As shown in figure 5, data processing unit 12 is defeated including data acquisition subelement 13, delay revise subelemen 14 and coordinate
Go out subelement 15, data acquisition subelement 13 receives millimetre-wave radar 1 and measures its obtained distance value ρ with target, connects simultaneously
The vertical rotary angle α and rotate horizontally angle beta that single-chip microcomputer sends, and millimetre-wave radar 1 scan angle theta of itself are received, so as to obtain
The position of complete millimetre-wave radar data and the plane of scanning motion；As shown in figure 5, set a certain target 17 that millimetre-wave radar 1 measures
Reading be (ρ, α, β, θ), and define：α=0 ° when millimetre-wave radar 1 is horizontal, when millimetre-wave radar 1 is in water
α values is just, α values are negative when millimetre-wave radar 1 is horizontal lower section when prosposition puts top；When the second rotary shaft 4 is with slowing down
β=0 ° when direction is vertical immediately ahead of device, when millimetre-wave radar 1 is located at the right side of β=0 °, β is on the occasion of when millimetre-wave radar 1
β is negative value during positioned at the left side of β=0 °；When itself scanning direction of millimetre-wave radar 1 is vertical with the place plane of millimetre-wave radar 1
When θ=0 °, when itself scanning direction is located at the top of θ=0 ° θ be on the occasion of when itself scanning direction is located at the lower section of θ=0 °
When θ be negative value.The anglec of rotation β of the first rotary shaft 3 is the anglec of rotation of millimetre-wave radar 1 in the horizontal direction as shown in Figure 3.
Preferably, delay effect refers to, because the present apparatus is using the technical scheme of three dimensionality dual rotary, therefore in thunder
Up to detection ripple during be issued to return, the position of radar has occurred that certain skew, although this period is very short,
But when rotary speed is higher, the error of this part is still very important, this is that the present apparatus fills with the detection of other fixed radars
Put different place, it is therefore necessary to introduce special delay correction factor.Delay revise subelemen 14 is repaiied including range measurement
Positive module, horizontal sweep correcting module and vertical scanning correcting module：Range measurement correcting module, the survey for the value ρ that adjusts the distance
Value be directed to the amendment of delay effect in detections of radar ripple two-way process, and its modifying factor exported is：
When | α1+θ1| ＞ | α2+θ2| and | β1| ＞ | β2| when, illustrate that the rotation of device is towards the direction motion of target point
, the actual value now measured is less than normal, therefore above formula uses positive sign, now λρ＞ 1, otherwise use negative sign, now λρ＜ 1；Meanwhile
Due to t1-t2It is the value of a very little, therefore the specific correction value of this correcting module depends entirely on the swing circle T of motor, rotation
Turn faster T it is smaller, then correction factor with 1 poor absolute value it is bigger, it is on the contrary then smaller.
Vertical scanning correcting module, imitated for be directed to being delayed in detections of radar ripple two-way process to vertical rotary angle α
The amendment answered, its modifying factor exportedWhen | α1| ＞ | α2| when, above formula takes positive sign, otherwise takes
Negative sign；
Horizontal sweep correcting module, for carrying out being directed in detections of radar ripple two-way process the effect that is delayed to rotating horizontally angle beta
The amendment answered, its modifying factor exportedWhen | β1| ＞ | β2| when, above formula takes positive sign, otherwise
Take negative sign；
Wherein m is the maximum detectable range of millimetre-wave radar 1, and ρ≤m；For reaction detection target 17 and millimeter wave
Influence of the distance to delay effect between radar 1, target 17 be then delayed closer to millimetre-wave radar 1 it is smaller, otherwise delay it is bigger；
t1For the time sent to the detections of radar ripple of target 17, t2The time returned for detections of radar ripple, then | t1-t2| represent thunder
Time needed for being travelled to and fro between up to detection ripple between target 17 and millimetre-wave radar 1；t1For the horizontal rotation week of millimetre-wave radar 1
Phase, t2For the vertical swing circle of millimetre-wave radar 1；α1For t1When α values, α2For t2When α values；β1For t1When β value, β2For
t2When β value；θ1For t1When θ values, θ2For t2When θ values；T1=2s, T2=2.4s, sampling interval of millimetre-wave radar for 2 °/
s。
Coordinate exports subelement 15：The object space coordinate exported after the revise subelemen amendment that is delayed is：
Wherein,
Data processing unit also includes target RCS fluctuation characteristics measurement subelement, for the RCS sequence variations system to target
Number measures, and radar cross section (RCS) value characterizes the ability of reception antenna direction target echo, by measuring target
RCS fluctuation characteristics, which can contrast, determines different target types.
Complex target for being in optical region, it is assumed that it is made up of N number of scattering center, can according to radar scattering theory
Know, radar return can regard the echo Vector modulation of multi-scattering centers as, due to sight of each scattering center with respect to radar
Angle is different so that in Vector modulation, respective relative phase changes the fluctuations for causing echo signal amplitude, RCS at random
Value, which follows, also there are fluctuations.Therefore radar target RCS changes very sensitive, target RCS time sequences to the attitude angle of target
Row are substantially variable quantities of the RCS with azimuth of target, are a relief volumes, then the RCS of multi-scattering centers target is expressed as mesh
Mark azimuthal function：
Wherein, σiRepresent that i-th of scattering center RCS, α+θ represents target with respect to the azimuth of millimetre-wave radar, RiRepresent the
I scattering center is with respect to radar center distance；λ is the parameter being manually set；
Then RCS sequence variations coefficient is expressed as：Wherein σ (k) represents kth time detection
The RCS values of target, RCS serial meansSequence variations coefficient and azimuth are inputted as characteristic parameter
Target identification system is to complete the identification to target.
In this embodiment, new millimetre-wave radar three-dimensional environment sensory perceptual system is devised for deceleration device, so as to realize
180 ° of front horizontal and being scanned without dead angle for 180 ° of vertical direction cover, and economy and durability simple in construction, strong antijamming capability；Profit
Other parts are coordinated to realize Automatic Control function with step-by-step motor, it is easy to control accurate；For new-type rotating radar system
The characteristics of system and delay effect devise range measurement correcting module, horizontal sweep correcting module, vertical scanning correcting module
Deng correcting module so that the coordinate setting function of radar is more accurate, sets T1=2.5s, T2=2.8s, the sampling of millimetre-wave radar
At intervals of 1.3 °/s.Realizing that measurement error is less than 0.6% while detection without dead angle, measuring delay rate less than 0.3%, and
Real-time is stronger；Accurate Coordinate calculation method is given, is provided the foundation to automatically control with control errors；It is new for this
Rotation mechanism, employ new RCS fluctuation characteristic measurement apparatus so that the measurement of the RCS coefficient of variation is more accurate, to mesh
Mark is not more favourable；The size of the parts such as rotating disk, rotary shaft can flexibly be chosen as the case may be, be various different size of
The applicability of deceleration device provides condition；Substitute traditional light wave radar with millimetre-wave radar, when being propagated using atmospheric window
Decay it is small, influenceed by natural light and infrared source small, target can effectively be identified under atrocious weather situation, be
Safety traffic provides reliable guarantee, has the superiority such as high resolution, high accuracy, miniature antenna bore, achieves unexpected
Effect.
Embodiment 5：
A kind of automatic slow-down device with identification function as Figure 1-4, including deceleration device and installed in deceleration
Millimetre-wave radar three-dimensional environment sensory perceptual system on device；Millimetre-wave radar three-dimensional environment sensory perceptual system include millimetre-wave radar 1,
Rotation mechanism 10, control unit 11 and data processing unit 12；Rotation mechanism bag 10 includes the first rotary shaft 3, rotation
The rotary shaft 4 of disk 2 and second, the first rotary shaft 3 arrangement and affixed with the center of rotating disk 2 vertically, first rotary shaft 3 passes through
The driving rotation of first stepper motor 8；The horizontal set of the second rotary shaft 4 of rotation is driven in bearing block 5 by the second stepper motor 9
Interior, the bearing block 5 is fixed in rotating disk 2 by 2 support shafts arranged vertically 6；The midpoint of second rotary shaft 4
Connecting portion 7 is provided with, the connecting portion 7 is integrally formed perpendicular to the second rotary shaft 4 and with the second rotary shaft 4, millimetre-wave radar 1
It is vertical with connecting portion 7 affixed；Itself intrinsic plane of scanning motion of the millimetre-wave radar 1 is swept perpendicular to the place plane of rotating disk 2
Range angle is retouched as ± 30 °；The rotating disk 2 has an otch 16 in the side of arrangement support shaft 6, the straight line parallel where otch 16 in
Straight line where second rotary shaft 4, and any support shaft 6 and the distance of the place straight line of otch 16 are less than 50mm；The first step
The stepper motor 9 of stepper motor 8 and second is controlled by single-chip microcomputer, and single-chip microcomputer is used to receive control command, and by control command
It is converted into control signal and is sent to motor, while the goniometer turned over according to the initial position of device and two stepper motors calculates
The current location of rotation mechanism, and the current position state of rotation mechanism 10 is fed back into data processing unit 12；
The cycle that the overall face forward 18 under the drive of the first stepper motor 8 of the rotation mechanism 10 does 180 ° of level comes and goes fortune
It is dynamic, while the face forward 20 under the drive of the second stepper motor 9 of millimetre-wave radar 1 does vertical 180 ° of cycle back and forth movement；
As shown in figure 5, data processing unit 12 is defeated including data acquisition subelement 13, delay revise subelemen 14 and coordinate
Go out subelement 15, data acquisition subelement 13 receives millimetre-wave radar 1 and measures its obtained distance value ρ with target, connects simultaneously
The vertical rotary angle α and rotate horizontally angle beta that single-chip microcomputer sends, and millimetre-wave radar 1 scan angle theta of itself are received, so as to obtain
The position of complete millimetre-wave radar data and the plane of scanning motion；As shown in figure 5, set a certain target 17 that millimetre-wave radar 1 measures
Reading be (ρ, α, β, θ), and define：α=0 ° when millimetre-wave radar 1 is horizontal, when millimetre-wave radar 1 is in water
α values is just, α values are negative when millimetre-wave radar 1 is horizontal lower section when prosposition puts top；When the second rotary shaft 4 is with slowing down
β=0 ° when direction is vertical immediately ahead of device, when millimetre-wave radar 1 is located at the right side of β=0 °, β is on the occasion of when millimetre-wave radar 1
β is negative value during positioned at the left side of β=0 °；When itself scanning direction of millimetre-wave radar 1 is vertical with the place plane of millimetre-wave radar 1
When θ=0 °, when itself scanning direction is located at the top of θ=0 ° θ be on the occasion of when itself scanning direction is located at the lower section of θ=0 °
When θ be negative value.The anglec of rotation β of the first rotary shaft 3 is the anglec of rotation of millimetre-wave radar 1 in the horizontal direction as shown in Figure 3.
Preferably, delay effect refers to, because the present apparatus is using the technical scheme of three dimensionality dual rotary, therefore in thunder
Up to detection ripple during be issued to return, the position of radar has occurred that certain skew, although this period is very short,
But when rotary speed is higher, the error of this part is still very important, this is that the present apparatus fills with the detection of other fixed radars
Put different place, it is therefore necessary to introduce special delay correction factor.Delay revise subelemen 14 is repaiied including range measurement
Positive module, horizontal sweep correcting module and vertical scanning correcting module：Range measurement correcting module, the survey for the value ρ that adjusts the distance
Value be directed to the amendment of delay effect in detections of radar ripple two-way process, and its modifying factor exported is：
When | α1+θ1| ＞ | α2+θ2| and | β1| ＞ | β2| when, illustrate that the rotation of device is towards the direction motion of target point
, the actual value now measured is less than normal, therefore above formula uses positive sign, now λρ＞ 1, otherwise use negative sign, now λρ＜ 1；Meanwhile
Due to t1-t2It is the value of a very little, therefore the specific correction value of this correcting module depends entirely on the swing circle T of motor, rotation
Turn faster T it is smaller, then correction factor with 1 poor absolute value it is bigger, it is on the contrary then smaller.
Vertical scanning correcting module, imitated for be directed to being delayed in detections of radar ripple two-way process to vertical rotary angle α
The amendment answered, its modifying factor exportedWhen | α1| ＞ | α2| when, above formula takes positive sign, otherwise takes
Negative sign；
Horizontal sweep correcting module, for carrying out being directed in detections of radar ripple two-way process the effect that is delayed to rotating horizontally angle beta
The amendment answered, its modifying factor exportedWhen | β1| ＞ | β2| when, above formula takes positive sign, otherwise
Take negative sign；
Wherein m is the maximum detectable range of millimetre-wave radar 1, and ρ≤m；For reaction detection target 17 and millimeter wave
Influence of the distance to delay effect between radar 1, target 17 be then delayed closer to millimetre-wave radar 1 it is smaller, otherwise delay it is bigger；
t1For the time sent to the detections of radar ripple of target 17, t2The time returned for detections of radar ripple, then | t1-t2| represent thunder
Time needed for being travelled to and fro between up to detection ripple between target 17 and millimetre-wave radar 1；t1For the horizontal rotation week of millimetre-wave radar 1
Phase, t2For the vertical swing circle of millimetre-wave radar 1；α1For t1When α values, α2For t2When α values；β1For t1When β value, β2For
t2When β value；θ1For t1When θ values, θ2For t2When θ values；T1=2s, T2=2.4s, sampling interval of millimetre-wave radar for 2 °/
s。
Coordinate exports subelement 15：The object space coordinate exported after the revise subelemen amendment that is delayed is：
Wherein,
Data processing unit also includes target RCS fluctuation characteristics measurement subelement, for the RCS sequence variations system to target
Number measures, and radar cross section (RCS) value characterizes the ability of reception antenna direction target echo, by measuring target
RCS fluctuation characteristics, which can contrast, determines different target types.
Complex target for being in optical region, it is assumed that it is made up of N number of scattering center, can according to radar scattering theory
Know, radar return can regard the echo Vector modulation of multi-scattering centers as, due to sight of each scattering center with respect to radar
Angle is different so that in Vector modulation, respective relative phase changes the fluctuations for causing echo signal amplitude, RCS at random
Value, which follows, also there are fluctuations.Therefore radar target RCS changes very sensitive, target RCS time sequences to the attitude angle of target
Row are substantially variable quantities of the RCS with azimuth of target, are a relief volumes, then the RCS of multi-scattering centers target is expressed as mesh
Mark azimuthal function：
Wherein, σiRepresent that i-th of scattering center RCS, α+θ represents target with respect to the azimuth of millimetre-wave radar, RiRepresent the
I scattering center is with respect to radar center distance；λ is the parameter being manually set；
Then RCS sequence variations coefficient is expressed as：Wherein σ (k) represents kth time detection
The RCS values of target, RCS serial meansSequence variations coefficient and azimuth are inputted as characteristic parameter
Target identification system is to complete the identification to target.
In this embodiment, new millimetre-wave radar three-dimensional environment sensory perceptual system is devised for deceleration device, so as to realize
180 ° of front horizontal and being scanned without dead angle for 180 ° of vertical direction cover, and economy and durability simple in construction, strong antijamming capability；Profit
Other parts are coordinated to realize Automatic Control function with step-by-step motor, it is easy to control accurate；For new-type rotating radar system
The characteristics of system and delay effect devise range measurement correcting module, horizontal sweep correcting module, vertical scanning correcting module
Deng correcting module so that the coordinate setting function of radar is more accurate, T1=2.6s, T2=2.9s, the sampling interval of millimetre-wave radar
For 1.2 °/s, realizing that measurement error is less than 0.5%, and measurement delay rate is less than 0.2% while detection without dead angle, and in real time
Property is stronger；Accurate Coordinate calculation method is given, is provided the foundation to automatically control with control errors；For the Novel rotary
Mechanical device, employ new RCS fluctuation characteristic measurement apparatus so that the measurement of the RCS coefficient of variation is more accurate, and target is known
Not it is more favourable；The size of the parts such as rotating disk, rotary shaft can flexibly be chosen as the case may be, be various different size of decelerations
The applicability of device provides condition；Substitute traditional light wave radar, declining when being propagated using atmospheric window with millimetre-wave radar
Reduce, influenceed by natural light and infrared source small, target can effectively be identified under atrocious weather situation, for safely
Traveling provides reliable guarantee, has the superiority such as high resolution, high accuracy, miniature antenna bore, achieves unexpected effect.
Finally it should be noted that the above embodiments are merely illustrative of the technical solutions of the present invention, rather than the present invention is protected
The limitation of scope is protected, although being explained with reference to preferred embodiment to the present invention, one of ordinary skill in the art should
Work as understanding, technical scheme can be modified or equivalent substitution, without departing from the reality of technical solution of the present invention
Matter and scope.
Claims (1)
1. a kind of automatic slow-down device with identification function, it is characterized in that, including deceleration device and on deceleration device
Millimetre-wave radar three-dimensional environment sensory perceptual system；Millimetre-wave radar three-dimensional environment sensory perceptual system includes millimetre-wave radar, whirler
Tool device, control unit and data processing unit；Rotation mechanism includes the first rotary shaft, rotating disk and the second rotary shaft,
First rotary shaft vertically arrangement and it is affixed with the center of rotating disk, first rotary shaft is revolved by the first driving stepper motor
Turn；The second rotation axis horizontal rotated by the second driving stepper motor is sleeved in bearing block, and the bearing block is vertical by 2
The support shaft of arrangement is affixed on the rotating pan；The midpoint of second rotary shaft is provided with connecting portion, and the connecting portion is vertical
It is integrally formed in the second rotary shaft and with the second rotary shaft, millimetre-wave radar is vertical with connecting portion affixed；The millimetre-wave radar
Itself intrinsic plane of scanning motion where the rotating disk plane, and scanning range angle is ± 30 °；The rotating disk is in arrangement branch
There is otch the side of support axle, and the straight line parallel where otch is in the straight line where the second rotary shaft, and any support shaft and otch
The distance of place straight line is less than 50mm；First stepper motor and the second stepper motor are controlled by single-chip microcomputer, monolithic
Machine is used to receive control command, and control command is converted into control signal and is sent to motor, while according to the initial bit of device
Put the current location that the goniometer turned over two stepper motors calculates rotation mechanism, and by the current of rotation mechanism
Location status feeds back to data processing unit；The overall face forward under the drive of the first stepper motor of the rotation mechanism
The cycle back and forth movement of 180 ° of level is done, while millimetre-wave radar face forward under the drive of the second stepper motor is done vertically
180 ° of cycle back and forth movement；
Data processing unit includes data acquisition subelement, delay revise subelemen and coordinate output subelement；Data acquisition
Unit receives its distance value ρ with target that millimetre-wave radar measurement obtains, while receives the vertical rotary angle α of single-chip microcomputer transmission
With horizontal rotation angle beta, and itself scan angle theta of millimetre-wave radar；If millimetre-wave radar to the reading of a certain target for (ρ, α,
β, θ), and define：α=0 ° when radar is horizontal, when radar is horizontal top, α values are just, at radar
α values are negative when below horizontal level, β=0 ° when the second rotary shaft is vertical with direction immediately ahead of deceleration device, when radar position
β is on the occasion of when radar is located at the left side of β=0 °, β is negative value when the right side of β=0 °；When itself scanning of millimetre-wave radar
θ=0 ° when plane where direction and millimetre-wave radar is vertical, when itself scanning direction be located at the top of θ=0 ° θ on the occasion of, when
θ is negative value when itself scanning direction is located at the lower section of θ=0 °；
Delay revise subelemen includes range measurement correcting module, horizontal sweep correcting module and vertical scanning correcting module：Away from
From measurement correcting module, the measured value for the value ρ that adjusts the distance repaiied for delay effect in detections of radar ripple two-way process
Just, the modifying factor of its output is：
When | α1+θ1| ＞ | α2+θ2| and | β1| ＞ | β2| when, above formula takes positive sign, otherwise takes negative sign；
Vertical scanning correcting module, for be directed to delay effect in detections of radar ripple two-way process to vertical rotary angle α
Amendment, its modifying factor exportedWhen | α1| ＞ | α2| when, above formula takes positive sign, otherwise takes negative
Number；
Horizontal sweep correcting module, for be directed to delay effect in detections of radar ripple two-way process to rotating horizontally angle beta
Amendment, its modifying factor exportedWhen | β1| ＞ | β2| when, above formula takes positive sign, otherwise takes negative
Number；
Wherein m is the maximum detectable range of millimetre-wave radar, and ρ≤m；For reaction detection target and millimetre-wave radar it
Between influence of the distance to delay effect, target be then delayed closer to radar it is smaller, otherwise delay it is bigger；t1For to the target radar
The time that detection ripple is sent, t2The time returned for detections of radar ripple；|t1-t2| represent detections of radar ripple travel to and fro between target and
Time needed between radar；T1For the horizontal rotation cycle of millimetre-wave radar, T2For the vertical swing circle of millimetre-wave radar；
α1For t1When α values, α2For t2When α values；β1For t1When β value, β2For t2When β value；θ1For t1When θ values, θ2For t2When θ
Value；T1=2s, T2=2.4s, the sampling interval of millimetre-wave radar is 2 °/s；
Coordinate exports subelement：The object space coordinate exported after the revise subelemen amendment that is delayed is：
Wherein,
Data processing unit also includes target RCS fluctuation characteristics measurement subelement, for entering to the RCS sequence variations coefficients of target
Row measurement：
Complex target for being in optical region, it is assumed that be made up of N number of scattering center, then the RCS tables of multi-scattering centers target
It is shown as the function of azimuth of target：
Wherein, σiRepresent that i-th of scattering center RCS, α+θ represents target with respect to the azimuth of millimetre-wave radar, RiRepresent i-th
Scattering center is with respect to radar center distance；λ is the parameter being manually set；
Then RCS sequence variations coefficient is expressed as：Wherein σ (k) represents kth time detection target
RCS values, RCS serial means
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| CN203398298U (en) * | 2013-08-27 | 2014-01-15 | 中船重工鹏力（南京）大气海洋信息系统有限公司 | A weather radar antenna rotary table |
| CN104977171A (en) * | 2015-07-01 | 2015-10-14 | 奇瑞汽车股份有限公司 | Device for detecting dead-zone monitoring system controller and control method thereof |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE20105340U1 (en) * | 2001-03-26 | 2001-07-26 | Daimler Chrysler Ag | Dimensional environment detection |
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Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN202171644U (en) * | 2011-06-22 | 2012-03-21 | 北京华远凌进电子科技有限公司 | Portable civil imaging monitoring radar and radar system |
| CN202669614U (en) * | 2012-04-12 | 2013-01-16 | 北京电子科技职业学院 | Anti-collision warning and automatic deceleration device of vehicle |
| CN202952942U (en) * | 2012-12-27 | 2013-05-29 | 巫溪县文峰职业中学校 | Automatic speed reduction device |
| CN203398298U (en) * | 2013-08-27 | 2014-01-15 | 中船重工鹏力（南京）大气海洋信息系统有限公司 | A weather radar antenna rotary table |
| CN104977171A (en) * | 2015-07-01 | 2015-10-14 | 奇瑞汽车股份有限公司 | Device for detecting dead-zone monitoring system controller and control method thereof |
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