CN207924174U - Sounding rocket detection system - Google Patents
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- CN207924174U CN207924174U CN201820293178.3U CN201820293178U CN207924174U CN 207924174 U CN207924174 U CN 207924174U CN 201820293178 U CN201820293178 U CN 201820293178U CN 207924174 U CN207924174 U CN 207924174U
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Abstract
The utility model provides a kind of sounding rocket detection system, belongs to vehicle-mounted sounding rocket lift-off technology field, which includes transmitting transport vehicle and command communication vehicle；Emit transport vehicle to assemble rocketsonde, carrier rocket and launch vehicle measurement；Command communication vehicle repaiies equipment, data receiver processing equipment and communication equipment to assemble wind；Wind repaiies equipment to calculate the firing attitude signal of carrier rocket according to external environment information, data receiver processing equipment can at least receive the data information of rocketsonde, the survey wind sonde of carrier rocket, weather station, and will be transmitted to base station by communication equipment after the processing data information.System hardware integrated level, the high degree of automation can realize " transmitting is integrated with transport, communication for command is integrated with data processing ", simplify the complete amount of system equipment group, reduce construction scale, improve the mobility of system and complete the independence of task.
Description
Technical field
The utility model is related to atmospheric sounding techniques fields, and in particular to a kind of sounding rocket detection system.
Background technology
Sounding rocket is sent payload to high-altitude using rocket as power, to the meteorological element or sky of terrestrial space
Between environmental element carry out in-situ investigation.According to payload or the difference of detection mission, it is divided into meteorological rocket, geophysics fire
Arrow, Bioexperiment rocket, nuclear test rocket, space technology test rocket and microgravity experiment rocket etc..Make a general survey of countries in the world fire
Arrow technology development course, all experienced the stage that sounding rocket is known the real situation as technology.The first type sounding rocket is beautiful in the world
State is in " corporal woman soldier " meteorological rocket emitted to October 25 on the 26th of September in 1945.Hereafter main military power of the world is flourishing
Develop rocket sounding technology, the especially U.S. transmits thousands of pieces of meteorological rockets in six the seventies of last century, obtains big
Measured data is measured, is established for the foundation of global standards air, Middle and upper atmosphere Context aware, near space vehicle development test etc.
Solid foundation.The United States, Russia etc. still meets meteorological support need in space launch, missile armament experiment using sounding rocket at present
It asks.
Sounding rocket detection system refers exclusively to the meteorological rocket sounding system detected to earth atmosphere meteorological element.Sounding
Rocket sounding system is generally made of payload, carrier rocket, launching site and four major part of Deep space tracking measuring station.With being
Using bead thermistor temperature sensor sonde and parachute as payload as unified；Using solid engines without control
Rocket is as carrier rocket；Launching site is selected in guided missile space experiment target range, is emitted using fixed launcher；Deep space tracking
Measuring station uses the fixed high-precision instrumentation control radar in target range, carries out track and localization to parachute, is connect using dedicated meteorological data
The sounding code that receiving unit is beamed back in ground receiver sonde.
At present sounding rocket detection system have the following disadvantages：
System hardware integrated level, the degree of automation be not high.With system composition equipment as emitter, tracking radar, specially
Effective integration is not carried out with meteorological detection data ground receiving equipment etc..When being detected, since system respectively forms equipment function
It is single, deployment scattered band is big, need to borrow the communication equipment outside this system, carry out unified command scheduling, could be harmonious complete
At work, detection operations efficiency is influenced.
Utility model content
The purpose of this utility model is to provide a kind of sounding rocket detection system, the sounding rocket detection system is integrated
Degree is high, manipulation is flexible, is suitable for various complex environments, and work efficiency is high.
Based on above-mentioned purpose, sounding rocket detection system provided by the utility model, including：Emit transport vehicle and commander is logical
Believe vehicle；
The transmitting transport vehicle is assembling rocketsonde, carrier rocket and launch vehicle measurement；
The rocketsonde is arranged inside the carrier rocket；
The launch vehicle measurement controls the delivery fire to receive the firing attitude signal that the command communication vehicle transmits
The firing attitude of arrow is simultaneously emitted；The command communication vehicle can also receive the firing attitude signal of launch vehicle measurement feedback；
And adjust the firing attitude for surveying hair empty set system for carrier rocket again according to feedback firing attitude signal；
The command communication vehicle repaiies equipment, data receiver processing equipment and communication equipment to assemble wind；
The wind repair equipment to according to external environment information calculate carrier rocket firing attitude signal,
The data receiver processing equipment can at least receive rocketsonde, the survey wind sonde of carrier rocket, meteorology
The data information stood, and base station will be transmitted to by communication equipment after the processing data information.
Further, the launch vehicle measurement includes launcher, general docking platform, launcher regulating device and control dress
It sets, the launcher is mounted on by launcher regulating device on general docking platform, and the general docking platform setting is being sent out
It penetrates on transport vehicle, the control device is connect with the launcher regulating device, launcher respectively.
Further, the transmitting transport vehicle includes carrier loader platform and protective device；The carrier loader platform includes driver's cabin
And vehicle frame, to install the survey hair empty set system, the protective device is arranged on the vehicle frame vehicle frame, and described anti-
Protection unit is between the launcher and the driver's cabin.
Further, the protective device includes protective plate and protective base；The protective plate connects with the protective base
It connects, the protective plate is set as inclined surface close to the end face of carrier rocket, and the inclined surface has inclined angle alpha with horizontal plane.
Further, the transmitting transport vehicle further includes heat preservation mechanism, and the heat preservation mechanism includes electric blower and leads to
Wind pipeline；
The guider of the launcher has air outlet and air inlet；The electric blower by ventilation shaft with it is described
Air inlet is connected to, to convey hot gas into the guider.
Further, the command communication vehicle includes vehicle frame and cabin, and the communication equipment, described is installed in the cabin
Data receiver processing equipment, power supply unit and the wind repair equipment.
Further, the command communication vehicle further includes parking bearing, and the parking bearing is arranged on vehicle frame.
Further, further include monitoring system, the monitoring system includes surveillance camera；The surveillance camera includes
Infrared probe, monitor, digital hard disc video recorder, the infrared probe, monitor are mounted on transmitting transport vehicle and communication for command
Che Shang, the digital hard disc video recorder are mounted on command communication vehicle to receive the number of the infrared probe and the monitor
Communication ceases.
Further, further include positioning and directing equipment, the positioning and directing equipment is arranged on the transmitting transport vehicle, institute
Positioning and directing equipment is stated to transmit the transmitting longitude and latitude of transport vehicle, height above sea level to the launch vehicle measurement and towards letter
Number.
Further, further include command communication vehicle positioning device, the command communication vehicle positioning device is arranged in the finger
It waves on communication truck, the command communication vehicle positioning device is transmitting the longitude and latitude of the command communication vehicle to the launch vehicle measurement
Degree, altitude signal.
Using above-mentioned technical proposal, the technique effect of sounding rocket detection system provided by the utility model has：
Sounding rocket detection system hardware integration degree, the high degree of automation.This system is in line with " transmitting and transport one
Change, communication for command it is integrated with data processing " design principle, by each system optimization combination, comprehensive integration to two vehicles, general
It was dispersed in the past and executes the composition equipment of detection mission in tens kilometer ranges jointly and focus on two at a distance of 100 meters~150 meters
Vehicle on, enormously simplify the complete amount of system equipment group, reduce construction scale, improve the mobility of system and complete task
Independence.
, manipulation high with system integration degree flexibly, be suitable for various complex environments, the characteristics of work efficiency is high.
Description of the drawings
It, below will be right in order to illustrate more clearly of specific embodiment of the present invention or technical solution in the prior art
Specific implementation mode or attached drawing needed to be used in the description of the prior art are briefly described, it should be apparent that, it is described below
In attached drawing be that some embodiments of the utility model are not paying creativeness for those of ordinary skill in the art
Under the premise of labour, other drawings may also be obtained based on these drawings.
Fig. 1 is the schematic diagram for the sounding rocket detection system that the utility model embodiment provides；
Fig. 2 is the structural schematic diagram for the transmitting transport vehicle that the utility model embodiment provides；
Fig. 3 is the vertical view for the transmitting transport vehicle that the utility model embodiment provides；
Fig. 4 is the structural schematic diagram of the protective device in the transmitting transport vehicle that the utility model embodiment provides；
Fig. 5 is the structural schematic diagram of the electric heating mechanism in the transmitting transport vehicle that the utility model embodiment provides；
Fig. 6 is the structural schematic diagram for the command communication vehicle that the utility model embodiment provides；
Fig. 7 is the rear structure schematic diagram for the command communication vehicle that the utility model embodiment provides.
Reference numeral：1- rocketsondes；2- carrier rockets；3- wind repaiies equipment；4- data receiver processing equipments；5- is communicated
Equipment；6- launchers；The general docking platforms of 7-；8- launcher regulating devices；9- protective devices；10- protective plates；The anti-river bottom protection of 11-
Seat；12- electric blowers；13- ventilation shafts；14- shells；15- air blowers；16- electric heating mechanisms；17- self-regulated leveling devices；
18- cabins；19- power supply units；20- parkings support.
Specific implementation mode
The technical solution of the utility model is clearly and completely described below in conjunction with attached drawing, it is clear that described
Embodiment is the utility model a part of the embodiment, instead of all the embodiments.Based on the embodiments of the present invention, originally
The every other embodiment that field those of ordinary skill is obtained without making creative work, belongs to this practicality
Novel protected range.
It is in the description of the present invention, it should be noted that term "center", "upper", "lower", "left", "right", " perpendicular
Directly ", the orientation or positional relationship of the instructions such as "horizontal", "inner", "outside" is to be based on the orientation or positional relationship shown in the drawings, and is only
The utility model and simplifying describes for ease of description, do not indicate or imply the indicated device or element must have it is specific
Orientation, with specific azimuth configuration and operation, therefore should not be understood as limiting the present invention.In addition, term " the
One ", " second ", " third " are used for description purposes only, and are not understood to indicate or imply relative importance.
In the description of the present invention, it should be noted that unless otherwise clearly defined and limited, term " is pacified
Dress ", " connected ", " connection " shall be understood in a broad sense, for example, it may be being fixedly connected, may be a detachable connection, or integrally
Connection；It can be mechanical connection, can also be electrical connection；Can be directly connected, can also indirectly connected through an intermediary,
It can be the connection inside two elements.For the ordinary skill in the art, it can understand above-mentioned art with concrete condition
The concrete meaning of language in the present invention.
It please refers to shown in Fig. 1-Fig. 3, sounding rocket detection system provided by the utility model, including：Emit transport vehicle and
Command communication vehicle；
Emit transport vehicle to assemble rocketsonde 1, carrier rocket 2 and launch vehicle measurement；
Rocketsonde 1 is arranged inside carrier rocket 2；
Launch vehicle measurement controls the transmitting appearance of carrier rocket 2 to receive the firing attitude signal of command communication vehicle transmission
State is simultaneously emitted；Command communication vehicle can also receive the firing attitude signal of launch vehicle measurement feedback；And emitted according to feedback
Attitude signal adjusts firing attitude of the launch vehicle measurement for carrier rocket 2 again；
Please refer to Fig. 6 and Fig. 7, command communication vehicle is repaiied equipment 3, data receiver processing equipment 4 and communication assembling wind and set
Standby 5；
Wind repair equipment 3 to according to external environment information calculate carrier rocket 2 firing attitude signal,
Data receiver processing equipment 4 at least can receive rocketsonde 1, wind repaiies survey wind sonde, the weather station of equipment 3
Data information, and base station will be transmitted to by communication equipment 5 after processing data information.
Please refer to Fig. 2, in a preferred embodiment, launch vehicle measurement includes launcher 6, general docking platform 7, transmitting
Frame regulating device 8 and control device, the above-mentioned component in addition to control device are alternatively referred to as launcher servo mechanism, and launcher 6 is logical
Launcher regulating device 8 to be crossed to be removably mounted on general docking platform 7, general docking platform 7 is arranged on transmitting transport vehicle,
Control device is electrically connected with launcher regulating device 8, launcher 6 respectively.What control device transmitted to receive command communication vehicle
Firing attitude signal, control launcher regulating device 8 and launcher 6, and then the firing attitude of carrier rocket 2 is adjusted
And emitted；The attitude signal of launcher 6 can also be fed back to command communication vehicle by control device, subsequently adjust again
It is whole.
Above-mentioned firing attitude signal includes mainly launch time and the angle of departure of rocket.
Specifically, control device sends predetermined angle control signal, adjustment to launcher servo mechanism in launch vehicle measurement
The launch angle of rocket, meanwhile, launcher servo mechanism feeds back the pre-configured orientation angle reached, pitching angle signal to control device,
Control device repaiies the information of the transmission of equipment 3 according to wind, after adjusting launch angle and pitch angle, is sent out again to launcher servo mechanism
Rear angle control signal is repaiied in air-supply.
Above-mentioned control device can also send transmitting ignition signal to launcher 6, and control rocket is emitted.
In addition, control device can also send main power source by wireless data transmission mode to rocketsonde 1 opens letter
Number.It is worked with waking up rocketsonde 1.
Survey hair control subsystem provided herein is to use general different from the place of traditional launch vehicle measurement
Docking platform is suitable for transmitting different model rocket.For the rocket of different size and length, such as expanding falling sphere detection
Rocket, only need to change guider can (i.e. guider is detachable, be connected to transmitting transport vehicle launcher 6 on), ensure that
The versatility of launcher 6.
Please refer to Fig. 2 and Fig. 4, in a preferred embodiment, transmitting transport vehicle includes carrier loader platform and protective device 9；
Carrier loader platform includes driver's cabin and vehicle frame, and vehicle frame surveys hair empty set system, i.e., the general docking platform 7 in launch vehicle measurement to install
On vehicle frame, protective device 9 is arranged on vehicle frame, and protective device 9 is between launcher 6 and driver's cabin.
The height on 9 top of protective device is higher than the height on the top for the launcher 6 being horizontal.
The height of protective device 9 and launcher 6 uses above-mentioned set-up mode, and protective device 9 can be made to be covered along short transverse
Lid launcher 6 (i.e. internal carrier rocket 2), fully protects driver's cabin.
In one preferred embodiment, the width of protective device 9 is adapted to the width of driver's cabin.It can make protective device 9
Launcher 6 is covered in the vehicle width direction, ensures the abundant protection to driver's cabin.
In one preferred embodiment, protective device 9 includes protective plate 10 and protective base 11；Protective plate 10 and anti-river bottom protection
Seat 11 connects, and protective plate 10 is set as inclined surface close to the end face of carrier rocket 2, and inclined surface has inclined angle alpha with horizontal plane.
The protective plate 10 preferably uses the steel plate of rectangle or square, has certain thickness, so that the steel plate
It can bear to be unlikely to damage driver's cabin to rocket impact force.Protective base 11 is welded or is bolted on
On the crossbeam of frame chassis, guarantee is capable of providing enough support strengths, can be by welding between pedestal and steel plate
Connection can also use for example bolted detachable connection, and above-mentioned protective plate 10 and protective base 11 detachably connect
It connects, convenient to protective plate 10, either protective base 11 is assembled or replaced.
Above-mentioned inclined angle alpha is preferably arranged to 50 degree of -85 degree, and inclined surface and the horizontal plane of protective plate 10 have inclined angle alpha,
Purpose is shock wave can be made to hoist pressure release along inclined surface at the inclined surface of rocket crash plate 10, is prevented to driving
Room damages, and reduces unnecessary loss.
Please refer to Fig. 2 and Fig. 5, in a preferred embodiment, transmitting transport vehicle further includes heat preservation mechanism, heat preservation mechanism packet
Include electric blower 12 and ventilation shaft 13；
Guider in launcher 6 has air outlet and air inlet；Electric blower 12 passes through ventilation shaft 13 and air inlet
Mouth connection, to convey hot gas into guider.
In one preferred embodiment, electric blower 12 includes shell 14 and the air blower being arranged in shell 14
15 and electric heating mechanism 16, the air outlet in face air blower 15 is arranged in electric heating mechanism 16, the air warp that air blower 15 exports
Electric heating mechanism 16 is delivered to by ventilation shaft 13 inside guider after heating.
For air blower 15 to output gas flow, the air outlet in air blower 15 is arranged in electric heating mechanism 16, and air blower 15 exports
Air-flow by forming hot wind after air blower 15, be input in guider by ventilation shaft 13, to rocket in guider into
Row heating and thermal insulation, it is ensured that sonde battery can work normally under low temperature environment.
In one preferred embodiment, electric heating mechanism 16 includes heating wire.Heating wire have simple in structure, fever is fast,
The characteristics of being easily installed and safeguarding.
In one preferred embodiment, air outlet is arranged in guider by the position of front end, and air inlet setting is being led
To the position close to middle rear end of device.
In above-mentioned technical proposal, air outlet and air inlet are successively set on the position by front end, middle rear end of guider,
Flowing stroke of the thermal current in guider can be ensured, to the rocketsonde of rocket and its carrying in guider electricity
Pond is in stable temperature environment.
In one preferred embodiment, transmitting transport vehicle further includes self-regulated leveling device 17, and self-regulated leveling device is existed using setting
On vehicle frame.
Self-regulated leveling device 17 has the telescopic supporting rod towards ground supports to carry out leveling to car body.Utilize the self-level(l)ing
Device facilitates the height for each position for adjusting car body, so that general docking platform 7 is in horizontality, is sent out for sounding rocket
It penetrates and brings safety guarantee.
Hydraulic telescopic rod, electric telescopic rod may be used in the self-regulated leveling device.Parking bearing 20 uses above-mentioned each type,
Have the characteristics that it is simple in structure, be easily installed and regulate and control.
When concrete application, which is electrically connected with control device in launch vehicle measurement, and control device can be to certainly
Levelling device sends leveling and controls signal, meanwhile, the water for the frame chassis that control device can also be fed back received from levelling device
Pingdu feedback signal, to ensure the levelness of frame chassis.
Please refer to Fig. 6 and Fig. 7, in a preferred embodiment, command communication vehicle includes vehicle frame and cabin 18, cabin 18
Upper installation communication equipment 5, data receiver processing equipment 4, power supply unit and wind repair equipment 3.
Communication equipment 5 includes vehicle radio station, satellite communication equipment 5, Beidou subscriber machine and sonde wireless remote control device.It should
Communication equipment 5 is used for when march is implemented to detect with position on the way, under command communication vehicle, transmitting transport vehicle and vehicle between personnel
It communicates (such as real time phone call)；The communication (voice, data file, image) being additionally operable between command communication vehicle and higher level command centre
It is realized by satellite communication equipment 5, and is additionally operable to receive and dispatch Big Dipper short message by Beidou subscriber machine, using as emergency backup hand
Section.Sonde wireless remote control device is mainly used to control sonde.
In one preferred embodiment, data receiver processing equipment 4 includes the sounding signal receiving antenna of electrical connection, sounding
Signal receives and demodulating unit, signal adapter, data processing terminal, ups power.The data receiver processing equipment 4 can connect
Receive what bottom surface weather information, the position data of observing and controlling sonde transmission and the rocketsonde 1 that automatic weather station is sent were sent
The monitor video signal that position, temperature, air pressure initial data, monitoring device are sent, through temperature adjustmemt and atmospheric density, air pressure,
After wind direction and wind velocity calculates, final detection product (comprising monitor video, measurement data, chart-information) is generated, through communication equipment 5
(data transmission set in attached drawing) is sent to higher level command centre (base).Connect wind repaiies subsystem to its reception antenna simultaneously.
Difference lies in can receive processing navigation simultaneously with the prior art for data receiver processing equipment 4 provided herein
Satellite positioning surveys wind sonde and 1 data of rocketsonde.So that level of integrated system improves, a set of ground installation is reduced, and
It is separated using frequency point, 3 sonde data can be received simultaneously, and do not interfere with each other.
In one preferred embodiment, wind repair equipment 3 include Earth Surface Automatic Weather Station, navigation satellite positioning survey wind devices,
Wind repaiies processing module.
Earth Surface Automatic Weather Station include ultrasonic wind detection sensor, temperature sensor, atmosphere pressure sensor, humidity sensor,
Data acquisition module and data processing module, Earth Surface Automatic Weather Station both be used for monitor Surface Meteorological variation, be also used for for
Navigation satellite positioning surveys wind and provides surface wind observation (obtaining surface wind observation by ultrasonic wind detection sensor), is visited for rocket
Empty instrument 1 provides surface temperature data (obtaining surface temperature data by temperature sensor), barometric observation number before rocket launching
According to (pass through atmosphere pressure sensor obtain barometric observation data) comparison value, to judge that 1 temperature of rocketsonde, baroceptor be
It is no working properly.It includes meteorological balloon, high pressure helium gas cylinder, sonde and ground receiving equipment that wind devices are surveyed in navigation satellite positioning.
Sonde is made of navigation satellite locating module, battery and transmitting antenna, and ground receiving equipment is total with data receiver processing equipment 4
With.Rocketsonde 1 leads lower rising in the meteorological balloon full of helium, location data is sent back ground receiving equipment, again
Data processing equipment receives the wind speed and direction data product for being processed into ground to high-altitude 6km.Wind repaiies processing module, is used for base area
Face wind and upper-level winds, calculate wind-induced sounding rocket transmitting angle offset, and output adjusts the angle of departure to launching control equipment is surveyed, protects
Card rocket remains to reach scheduled height and speed under different upper-level winds launching conditions.
Wind provided herein repaiies being mainly characterized by for subsystem and uses the navigation of the simplification repaiied suitable for wind and defend
Wind devices are surveyed in star positioning.Balloon uses 100g meteorological balloons, and Blasting height is in 8km or more, it is ensured that 6km or less upper air wind findings need
It asks；High pressure helium gas cylinder uses 40L standard high-voltage bottles, meets 4 balloon inflation amount demands；Sonde is using conventional sonde
Simplify version, only navigation satellite locating module, applicator is using being suitble to vehicle-mounted automatic put ball device (low temperature or windy conditions
Lower enabling), high degree of automation.
Power supply unit 19 includes (considering low temperature in plateau for the independent electric power supply of transmitting transport vehicle and command communication vehicle configuration
Use environment need to configure low-temperature cool starting and turbocharging), the main rocket heat preservation for ensureing transmitting transport vehicle and emission control with
And on command communication vehicle each software and hardware system normal operation.
In one preferred embodiment, command communication vehicle further includes parking bearing 20, and parking bearing 20 is arranged on vehicle frame.
Parking bearing 20 has the telescopic supporting rod towards ground supports to be supported to car body.
Hydraulic telescopic rod, electric telescopic rod or jack may be used in parking bearing 20.Parking bearing 20 is using above-mentioned
Each type, have the characteristics that it is simple in structure, be easily installed and regulate and control.
When concrete application, the parking bearing 20 in launch vehicle measurement control device be electrically connected, control device can in
Vehicle bearing 20 sends expansion control signal, is supported with controlling parking 20 pairs of car bodies of bearing.
In one preferred embodiment, which further includes monitoring system, and monitoring system includes monitoring
Video camera；Surveillance camera includes infrared probe, monitor, digital hard disc video recorder, and infrared probe, monitor are mounted on transmitting
On transport vehicle and command communication vehicle, digital hard disc video recorder is mounted on command communication vehicle to receive infrared probe and monitor
Number communication breath.
In one preferred embodiment, which further includes positioning and directing equipment, positioning and directing equipment
On transmitting transport vehicle, positioning and directing equipment emits longitude and latitude, the height above sea level of transport vehicle to be transmitted to launch vehicle measurement for setting
Spend signal.
In one preferred embodiment, which further includes command communication vehicle positioning device, Zhi Huitong
Believe vehicle positioning device be arranged on command communication vehicle, command communication vehicle positioning device to launch vehicle measurement transmit communication for command
The longitude and latitude of vehicle, altitude signal.
Using sounding rocket detection system provided by the present application, rocket sounding is carried out, is had the following advantages：
1. system hardware integrated level, high degree of automation.This system in line with " transmitting with the integrated, communication for command of transport and
Data processing integration " design principle, it is several by being dispersed in the past by each system optimization combination, comprehensive integration to two vehicles
The composition equipment for executing detection mission in ten kilometer ranges jointly focuses on two on 100 meters~150 meters of vehicle, integrates
The degree of automation for improving equipment in journey as possible, enormously simplifies the complete amount of system equipment group, reduces construction scale, improves and is
The mobility of system and the independence for completing task.
2. transmitting is carried out integrated design with transport, rocket is placed in launcher 6 with arm-to-arm, both ensures transportational process
Middle rocket damping and safety, and conveniently released to the protection after launching site, and reduce by a missile transporting truck.
3. using the Big Dipper/GPS positioning sonde, location information is acquired with detection data and is sent simultaneously simultaneously, before overcoming
The shortcomings that location data and meteorological data are acquired, respectively sent respectively, reduces by a track and localization radar truck, and defend using navigation
Star timing function, location data and detection data timing code are highly consistent, system no longer design time unified device.
4. sounding signal receiving antenna uses pentahedron antenna array in data process subsystem, cut automatically according to signal gain
Front is received in changing-over, is not required to manually adjust antenna direction, is reduced by a post operation personnel.Sounding signal receiving antenna can connect simultaneously
It receives processing navigation satellite positioning and surveys wind sonde and 1 data of rocketsonde, reduce a set of ground installation, and frequency point can divide
It opens up and sets, 3 sonde data can be received simultaneously, and do not interfere with each other.
5. by communication for command and data processing integrated design, makes the forward commander of commanding, visual scheduling, improve
Detection operations efficiency, penetrates that preceding detection, firing angle adjustment, transmitting, real-time detection data are shown, final products are shown and are sent and all referred to
It waves in personnel's grasp, is disposed convenient for case of emergency.
Finally it should be noted that：The above various embodiments is only to illustrate the technical solution of the utility model, rather than limits it
System；Although the utility model has been described in detail with reference to the foregoing embodiments, those skilled in the art should
Understand：It still can be with technical scheme described in the above embodiments is modified, either to which part or whole
Technical characteristic carries out equivalent replacement；And these modifications or replacements, this practicality that it does not separate the essence of the corresponding technical solution are new
The range of each embodiment technical solution of type.
Claims (10)
1. a kind of sounding rocket detection system, which is characterized in that including：Emit transport vehicle and command communication vehicle；
The transmitting transport vehicle is assembling rocketsonde, carrier rocket and launch vehicle measurement；
The rocketsonde is arranged inside the carrier rocket；
The launch vehicle measurement controls the carrier rocket to receive the firing attitude signal that the command communication vehicle transmits
Firing attitude is simultaneously emitted；The command communication vehicle can also receive the firing attitude signal of launch vehicle measurement feedback；And root
The firing attitude of carrier rocket is adjusted according to feedback firing attitude signal；
The command communication vehicle repaiies equipment, data receiver processing equipment and communication equipment to assemble wind；
The wind repair equipment to according to external environment information calculate carrier rocket firing attitude signal,
The data receiver processing equipment, which at least can receive rocketsonde, wind repaiies equipment surveys wind sonde, weather station
Data information, and base station will be transmitted to by communication equipment after the processing data information.
2. sounding rocket detection system according to claim 1, which is characterized in that the launch vehicle measurement includes transmitting
Frame, general docking platform, launcher regulating device and control device, the launcher are mounted on logical by launcher regulating device
With on docking platform, the general docking platform setting on transmitting transport vehicle, the control device respectively with the launcher
Regulating device, launcher connection.
3. sounding rocket detection system according to claim 2, which is characterized in that the transmitting transport vehicle includes that carrier vehicle is flat
Platform and protective device；The carrier loader platform includes driver's cabin and vehicle frame, and the vehicle frame is described to install the launch vehicle measurement
Protective device is arranged on the vehicle frame, and the protective device is between the launcher and the driver's cabin.
4. sounding rocket detection system according to claim 3, which is characterized in that the protective device include protective plate and
Protective base；The protective plate is connect with the protective base, and the protective plate is set as inclining close to the end face of carrier rocket
Inclined-plane, the inclined surface have inclined angle alpha with horizontal plane.
5. sounding rocket detection system according to claim 2, which is characterized in that the transmitting transport vehicle further includes heat preservation
Mechanism, the heat preservation mechanism include electric blower and ventilation shaft；
The guider of the launcher has air outlet and air inlet；The electric blower passes through ventilation shaft and the air inlet
Mouth connection, to convey hot gas into the guider.
6. sounding rocket detection system according to claim 1, which is characterized in that the command communication vehicle include vehicle frame and
Cabin installs the communication equipment, the data receiver processing equipment, power supply unit and the wind in the cabin and repaiies equipment.
7. sounding rocket detection system according to claim 6, which is characterized in that the command communication vehicle further includes parking
Bearing, the parking bearing are arranged on vehicle frame.
8. sounding rocket detection system according to claim 1, which is characterized in that further include monitoring system, the monitoring
System includes surveillance camera；The surveillance camera includes infrared probe, monitor, digital hard disc video recorder, described infrared
Probe, monitor are mounted on transmitting transport vehicle, and the digital hard disc video recorder is mounted on command communication vehicle to receive
State the number communication breath of infrared probe and the monitor.
9. sounding rocket detection system according to claim 1, which is characterized in that further include positioning and directing equipment, it is described
Positioning and directing equipment be arranged on the transmitting transport vehicle, the positioning and directing equipment to the launch vehicle measurement transmission institute
State the transmitting longitude and latitude of transport vehicle, height above sea level and towards signal.
10. sounding rocket detection system according to claim 1, which is characterized in that further include that command communication vehicle positioning is set
Standby, the command communication vehicle positioning device is arranged on the command communication vehicle, the command communication vehicle positioning device to
The launch vehicle measurement transmits the longitude and latitude of the command communication vehicle, altitude signal.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820293178.3U CN207924174U (en) | 2018-03-01 | 2018-03-01 | Sounding rocket detection system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820293178.3U CN207924174U (en) | 2018-03-01 | 2018-03-01 | Sounding rocket detection system |
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| Publication Number | Publication Date |
|---|---|
| CN207924174U true CN207924174U (en) | 2018-09-28 |
Family
ID=63601893
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| Application Number | Title | Priority Date | Filing Date |
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| CN201820293178.3U Active CN207924174U (en) | 2018-03-01 | 2018-03-01 | Sounding rocket detection system |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112327679A (en) * | 2020-10-12 | 2021-02-05 | 中国运载火箭技术研究院 | Ground measurement and launch control system |
| CN114629540A (en) * | 2022-03-01 | 2022-06-14 | 西安航天动力技术研究所 | Communication networking system of carrier system under field unsupported condition |
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2018
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Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112327679A (en) * | 2020-10-12 | 2021-02-05 | 中国运载火箭技术研究院 | Ground measurement and launch control system |
| CN114629540A (en) * | 2022-03-01 | 2022-06-14 | 西安航天动力技术研究所 | Communication networking system of carrier system under field unsupported condition |
| CN114629540B (en) * | 2022-03-01 | 2024-01-23 | 西安航天动力技术研究所 | Communication networking system of carrier system under field non-support condition |
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