CN107728498A - One kind recovery monitoring system - Google Patents
One kind recovery monitoring system Download PDFInfo
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- CN107728498A CN107728498A CN201710947536.8A CN201710947536A CN107728498A CN 107728498 A CN107728498 A CN 107728498A CN 201710947536 A CN201710947536 A CN 201710947536A CN 107728498 A CN107728498 A CN 107728498A
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- recovery
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- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05B—CONTROL OR REGULATING SYSTEMS IN GENERAL; FUNCTIONAL ELEMENTS OF SUCH SYSTEMS; MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS OR ELEMENTS
- G05B19/00—Programme-control systems
- G05B19/02—Programme-control systems electric
- G05B19/04—Programme control other than numerical control, i.e. in sequence controllers or logic controllers
Abstract
The invention discloses one kind to reclaim monitoring system.The system includes：Front end monitoring apparatus and ground monitoring device；The front end monitoring apparatus, it is laid on recovery carrier, for monitoring the status information of recovery carrier, the state data packets of the processing acquisition recovery carrier, and Real-time Feedback to the ground monitoring device；The ground monitoring device, is laid on ground control cabinet, for receiving the state data packets of the front end monitoring apparatus feedback, to monitor the state of flight of the recovery carrier in real time based on the state data packets.Utilize the system, the monitoring of real time status information can be carried out to the state of flight that carrier is reclaimed caused by emission system, it is achieved thereby that the recovery of recovery carrier high-efficiency, improves the organic efficiency for reclaiming carrier, and then the cost of recovery has been saved, reduce recovery carrier Loss Rate.
Description
Technical field
The present embodiments relate to monitoring technology field, more particularly to a kind of recovery monitoring system.
Background technology
Global positioning system (Global Positioning System GPS) has in sea, land and sky comprehensive real-time three
Dimension navigation and the new generation satellite navigation and alignment system of stationkeeping ability.Beidou satellite navigation system (BeiDou Navigation
Satellite System) it is independent development capability, the GPS of independent operating that China is implementing.
GPS/ triones navigation systems have been successfully applied to emission system field, such as the transmitting of guided missile.In MISSILE LAUNCHING mistake
Cheng Zhong, the substantial amounts of carrier to be recycled of the separation that can come off, such as the cylinder of guided missile.If the position and state of reclaiming carrier cannot be real
When monitoring, cannot be apparent from reclaim carrier state of flight, can not realize recovery carrier high efficiente callback, and then
Cause substantial amounts of economic loss.Therefore, most important is just become to the real-time monitoring for reclaiming carrier positions and status information.
The content of the invention
A kind of recovery monitoring system provided by the invention, realizes the status information to reclaiming carrier caused by emission system
Real-time monitoring.
The embodiments of the invention provide one kind to reclaim monitoring system, including：Front end monitoring apparatus and ground monitoring device；
The front end monitoring apparatus, it is laid on recovery carrier, for monitoring the status information of recovery carrier, processing obtains
The state data packets of the recovery carrier, and Real-time Feedback is to the ground monitoring device；
The ground monitoring device, is laid on ground control cabinet, for receiving the shape of the front end monitoring apparatus feedback
State packet, to monitor the state of flight of the recovery carrier in real time based on the state data packets.
The embodiments of the invention provide one kind to reclaim monitoring system, is monitored first by the front end being laid on recovery carrier
Device monitoring reclaims the status information of carrier, and processing obtains the state data packets of the recovery carrier, and Real-time Feedback is to described
Ground monitoring device；Then the front end monitoring apparatus is received by the ground monitoring device being laid on ground control cabinet to feed back
State data packets, with based on the state data packets monitor in real time it is described recovery carrier state of flight.Utilize above-mentioned technology
Scheme, the monitoring of real time status information can be carried out to the state of flight that carrier is reclaimed caused by emission system, it is achieved thereby that
The recovery of carrier high-efficiency is reclaimed, improves the organic efficiency of recovery carrier, and then has saved the cost of recovery, reduces recovery carrier
Loss Rate.
Brief description of the drawings
Fig. 1 is a kind of structural representation of recovery monitoring system in the embodiment of the present invention one；
Fig. 2 is the structural representation of another recovery monitoring system in the embodiment of the present invention two；
Fig. 3 is the structural representation of another recovery monitoring system in the embodiment of the present invention three.
Embodiment
The present invention is described in further detail with reference to the accompanying drawings and examples.It is understood that this place is retouched
The specific embodiment stated is used only for explaining the present invention, rather than limitation of the invention.It also should be noted that in order to just
Part related to the present invention rather than entire infrastructure are illustrate only in description, accompanying drawing.
Embodiment one
Fig. 1 is a kind of structural representation for recovery monitoring system that the embodiment of the present invention one provides, and the present embodiment is applicable
In situation about being monitored in real time to reclaiming carrier caused by emission system, the recovery monitoring system is made up of two devices,
It is laid in respectively on recovery carrier and on ground control cabinet.As shown in figure 1, the recovery monitoring system includes：Front end monitoring dress
10 and ground monitoring device 20 are put, wherein：
Front end monitoring apparatus 10, it is laid on recovery carrier, for monitoring the status information of recovery carrier, processing obtains institute
The state data packets of recovery carrier are stated, and Real-time Feedback is to ground monitoring device 20；
Ground monitoring device 20, is laid on ground control cabinet, the status number fed back for receiving front-end supervising device 10
According to bag, to monitor the state of flight of the recovery carrier in real time based on the state data packets.
In the present embodiment, the operation principle of the recovery monitoring system is：The front end monitoring dress being laid on recovery carrier
The status information of 10 monitorings recovery carrier, the state data packets of the processing acquisition recovery carrier, and Real-time Feedback are put to ground
Supervising device 20；Then the state for the receiving front-end supervising device 10 of ground monitoring device 20 feedback being laid on ground control cabinet
Packet, to monitor the state of flight of the recovery carrier in real time based on the state data packets.
Specifically, recovery monitoring system can be understood as position and the status information to reclaiming carrier caused by emission system
The system monitored in real time.Recovery carrier can be understood as in emission system emission process, and the separation that comes off needs to carry out
The carrier of recovery.The status information of the recovery carrier can be understood as characterizing the letter of recovery carrier movement state and sign state
Breath.Further, the motion state can be understood as reclaiming the information such as the speed of carrier, angular speed, direction；The sign shape
State can be understood as reclaiming the information such as acceleration, the temperature of carrier.The state data packets can be understood as having merged recovery load
The packet of all status informations of body.The state of flight can be understood as reclaiming the status information in carrier flight course.
In the present embodiment, reclaim monitoring system to be used to monitor the status information for reclaiming carrier in real time, so as to quick
Efficiently recovery carrier is reclaimed, moreover it can be used to which the state of carrier is reclaimed in ex-post analysis.Specifically, recovery carrier is by being laid in
Front end monitoring apparatus 10 on recovery carrier forms with the two parts of ground monitoring device 20 being laid on ground control cabinet.
Front end monitoring apparatus 10 is used to monitor the status information for reclaiming carrier in real time, and the status information is passed through and preset
Policies portfolios into state data packets, then can be in the form of binary in real time by the status information feedback of monitoring to ground
Supervising device 20；Ground monitoring device 20 is analyzed and processed to the state data packets received by default strategy, and can
The data after processing are shown in real time in the form of by data and/or curve, it is achieved thereby that to recovery carrier
The real-time monitoring of state of flight.
It is understood that front end monitoring apparatus 10 and ground monitoring device 20 can be carried out by way of being wirelessly transferred
The transmission of data.
A kind of recovery monitoring system that the embodiment of the present invention one provides, includes the front end monitoring being laid on recovery carrier
Device and the ground monitoring device being laid on ground control cabinet；The state that recovery carrier is monitored by front end monitoring apparatus is believed
Breath, processing obtains the state data packets of the recovery carrier, and Real-time Feedback is to the ground monitoring device；Pass through ground monitoring
Device receives the state data packets, to monitor the state of flight of the recovery carrier in real time based on the state data packets.Profit
, can be to the prison for the state of flight progress real time status information that carrier is reclaimed caused by emission system with above-mentioned recovery monitoring system
Control, it is achieved thereby that recovery carrier high-efficiency recovery, improve recovery carrier organic efficiency, and then saved recovery into
This, reduces recovery carrier Loss Rate.
Further, front end monitoring apparatus 10 includes：Satellite navigation monitoring module 110, Sensor monitoring module 120, in
Heart control module 130, the power module 150 of first data transmission module 140 and first；
Satellite navigation monitoring module 110, electrically connected with Central Control Module 130, monitor the actual shape of the recovery carrier
State information, and feed back to Central Control Module 130；
Sensor monitoring module 120, electrically connected with Central Control Module 130, the recovery carrier is arranged at for basis
On Sensor monitoring obtain the second status information, and feed back to Central Control Module 130；
Central Control Module 130, electrically connected with first data transmission module 140, for the virtual condition information from reception
Middle extraction first state information, and first state information that synchronization receives and the second status information are merged into place
Reason, obtain it is described recovery carrier the moment state data packets and feed back to first data transmission module 140；
First data transmission module 140, for the state data packets at the moment to be fed back into ground monitoring device 20；
First power module 150, for being controlled for satellite navigation monitoring module 110, Sensor monitoring module 120, center
Module 130 and first data transmission module 140 are powered.
Specifically, satellite navigation monitoring module 110 can be understood as the monitoring mould for monitoring recovery carrier movement state
Block.Satellite navigation monitoring module 110 can use GPS/ Beidou navigation monitoring modules.Corresponding, virtual condition information can manage
Solve as the status information containing GPS/ Big Dipper effective informations.Wherein, effective information can be understood as reclaiming needed for monitoring system
Movement state information.Sensor monitoring module 120 can be understood as the monitoring mould for monitoring recovery carrier sign state information
Block.Second status information can be understood as the sign state information for the recovery carrier that Sensor monitoring arrives.Central Control Module 130
The core processing control module of front end monitoring apparatus 10 is can be understood as, available for collection, processing and the fusion for carrying out data.
On this basis, Central Control Module 130 can include information acquisition unit, information process unit and information fusion
Unit (not shown).Specifically, information acquisition unit can be used for the reality for gathering the feedback of satellite navigation monitoring module 110
The first state information that status information and Sensor monitoring module 120 are fed back.Information process unit can be used for from virtual condition
First state information and the second status information of synchronization are extracted in information.Information fusion unit can be used for first state
Information and the second status information merge processing, to be recycled state data packets of the carrier at the moment.
First data transmission module 140 can be understood as the data transmit-receive module of front end monitoring apparatus 10.Can be by center
The state data packets obtained after the processing of control module 130 are transmitted to ground monitoring device 20.First power module 150 preferably can be with
It is satellite navigation monitoring module 110, Sensor monitoring module 120, the number of Central Control Module 130 and first for 12V lithium batteries
Powered according to transport module 140.It will be evident that the power supply can be understood as directly being powered to modules, it is understood that
To be powered indirectly to modules.For example, in the course of work of front end monitoring apparatus 10, the first power module 150 can be with
Control module 130 and first data transmission module 140 are powered centered on directly, satellite navigation monitoring module 110, sensor prison
Surveying module 120 can be powered by the power conversion unit set in Central Control Module 130.Wherein power conversion unit can be managed
Solve as the 12V of input to be converted to the power subsystem of 3.3V outputs.
In the present embodiment, the virtual condition information of carrier is reclaimed by the monitoring in real time of satellite navigation monitoring module 110,
And the virtual condition feedback of the information monitored to Central Control Module 130 is handled.It is real by Sensor monitoring module 120
When monitor and the second status information of recovery carrier, and feed back to Central Control Module 130 and handled.Wherein, the second state
Information is obtained by the Sensor monitoring being arranged on recovery carrier.Sensor monitoring module 120 can be not provided with sensing
Device.
On this basis, Central Control Module 130 is at the virtual condition information and the second status information that receive
Reason, to be recycled the state data packets of carrier.Specifically, Central Control Module 130 extracts institute from virtual condition information
The first state information needed, and the first state information of synchronization and the second status information are merged, it is same to obtain
Moment records the state data packets of body next time.Wherein, first state information can be understood as reclaiming the movement state information of carrier.
Central Control Module 130 feeds back to first data transmission module 140 after obtaining the state data packets of synchronization, with
By first data transmission module 140 by the status information feedback monitored in real time to ground monitoring device 20.
On the basis of above-described embodiment, ground monitoring device 20 includes：Second data transmission module 210, monitoring module
220 and second source module 230；
Second data transmission module 210, is electrically connected with monitoring module 220, is fed back for receiving front-end supervising device 10
State data packets, and feed back to monitoring module 220；
Monitoring module 220, for monitoring the state of flight of the recovery carrier in real time based on the state data packets；
Second source module 230, for being powered for the second data transmission module 210.
Specifically, the second data transmission module 210 can be understood as the data transmit-receive module of ground monitoring device 20.Can be with
The state data packets that receiving front-end supervising device 10 feeds back, and feed back to monitoring module 220 and be used to monitor the recovery in real time
The state of flight of carrier.Specifically, it can be monitored in real time by data and/or the form of curve.
Second source module 230 preferably can be 12V lithium batteries, be powered for the second data transmission module 210.It is appreciated that
, monitoring module 220 preferably can be industrial computer, and can select 220V AC-powereds.
Embodiment two
Fig. 2 is the structural representation for another recovery monitoring system that the embodiment of the present invention two provides, and the present embodiment is upper
State and optimize on the basis of each embodiment.In the present embodiment, by satellite navigation monitoring module 110, it is further detailed as：
At least two signal transmitting and receiving antennas 1101, combiner 1102 and signal receiver 1103.
At least two supported signal dual-mode antennas 1101, with different positions and pose be fixedly arranged on it is described recovery carrier on, respectively with combiner
1102 electrical connections, for receiving the signal data for the relevant recovery carrier that satellite navigation system is sent in different positions and pose, and
Feed back to combiner 1102；
Combiner 1102, electrically connected with signal receiver 1103, for being fed back at least two supported signal dual-mode antennas 1101
Signal data carry out fusion treatment, obtain the actual signal data of the recovery carrier, and feed back to signal receiver 1103；
Signal receiver 1103, electrically connected with Central Control Module 130, for being determined according to the actual signal data of reception
The virtual condition information of the recovery carrier, and Central Control Module 130 is fed back to, wherein, the virtual condition information includes：
Position, Velocity and Time information.
Specifically, at least two supported signal dual-mode antennas 1101 are it is to be understood that be received back to the reception for recording body signal data
Device.Different positions and pose can be understood as different positions and posture.Wherein, at least two supported signal dual-mode antennas 1101 are with different positions
Appearance is fixedly arranged on the recovery carrier, is to guarantee under each different positions and pose, is received satellite navigation system hair
The signal data of the relevant recovery carrier sent.Combiner can be understood as obtaining at least two supported signal dual-mode antennas 1101
Signal data fusion device.Actual signal data can be understood as reclaiming carrier signal number actual in flight course
According to.Signal receiver is appreciated that to calculate the device of Position, Velocity and Time information according to actual signal data.
In the present embodiment, at least two supported signal dual-mode antennas 1101 receive satellite navigation system transmission under different positions and pose
Signal data, acquire and the signal data fed back into the fusion that combiner 1102 carries out data after the signal data,
To be recycled carrier actual signal data.Then the actual signal data after fusion is fed back to signal and received by combiner 1102
Machine 1103, for determining the virtual condition information of recovery carrier.And by the virtual condition feedback of the information to Central Control Module
130 are handled.
Further, the present embodiment is embodied as also by Sensor monitoring module 120：Sensor monitoring interface 1201 with
And it is fixedly arranged on pressure sensor, acceleration transducer and the temperature sensor of the recovery carrier surface.
Sensor monitoring interface 1201, electrically connected with Central Control Module 130, for receiving the pressure sensor collection
Pressure information, the acceleration transducer collection acceleration information and the temperature sensor collection temperature information,
Form the second status information for feeding back to Central Control Module 130.
Specifically, Sensor monitoring interface 1201 can be sensor general-purpose interface.Can be by setting different voltage
The sensor type of access is set.
In the present embodiment, front end monitoring apparatus 10 can only set Sensor monitoring interface 1201, corresponding sensor
The recovery carrier surface can be fixedly arranged on.Sensor monitoring interface 1201 is receiving the pressure letter of pressure sensor collection
After the temperature information of breath, the acceleration information of acceleration transducer collection and temperature sensor collection, center control is fed back to
Module 130.As can be seen here, the second status information can be pressure, acceleration and the temperature that Sensor monitoring interface 1201 receives
Spend information.
On the basis of above-mentioned optimization, first data transmission module 140 is specifically optimized for：Include front end radio station day
The front end data radio station 1402 of line 1401, for the state data packets to be passed through into front end radio antenna in the form of data-signal
1401 feed back to ground monitoring device 20；By the second data transmission module 210, specifically it is optimized for：Include land station antenna
2101 ground data radio station 2102, for the data fed back by the receiving front-end radio antenna 1401 of land station antenna 2101
Signal, obtain state data packets corresponding to the data-signal and feed back to monitoring module 220.
Specifically, front end radio antenna 1401 can be understood as the device of signal transmitting and receiving in front end monitoring apparatus 10.Enter one
Step, the device of data signal transmission can be carried out between front end monitoring apparatus 10 and ground monitoring device 20.Front end number conducts electricity
Platform 1402 can be understood as the radio station carried out data transmission in front end monitoring apparatus 10.Land station antenna 2101 can be understood as
The device of signal transmitting and receiving in ground monitoring device 20.Land station antenna 2101 can be understood as carrying out in ground monitoring device 20
The radio station of data transfer.
In the present embodiment, when front end data radio station 1402 receives the state data packets of the feedback of Central Control Module 130
Afterwards, the state data packets are fed back to by ground monitoring device 20 by front end radio antenna 1401 in the form of data-signal.
When ground data radio station 2102 receives the data-signal by land station antenna 2101, status data corresponding to acquisition
Bag, and the state data packets are fed back into monitoring module 220 and carry out Treatment Analysis, the flight shape of carrier is reclaimed with real-time monitoring
State.
The structural representation for another recovery monitoring system that the embodiment of the present invention two provides, embodies satellite navigation prison
Control module, Sensor monitoring module, first data transmission module and the second data transmission module.Using the recovery monitoring system,
It can realize and carry out position, speed, time, pressure, acceleration and temperature to reclaiming carrier state of flight caused by emission system
Real-time monitoring, it is achieved thereby that the recovery of recovery carrier high-efficiency, improves the organic efficiency of recovery carrier, and then saved time
The cost of receipts, reduce recovery carrier Loss Rate.
Embodiment three
Fig. 3 show the structural representation of another recovery monitoring system of the offer of the embodiment of the present invention three, the present embodiment
Optimized on the basis of the various embodiments described above.Front end monitoring apparatus 10 also optimizes and included in the present embodiment：Information stores
Module 160, for reclaiming the status information and state data packets of carrier described in real-time storage.
, can be to reclaim carrier described in real-time storage specifically, front end monitoring apparatus 10 is additionally provided with information storage module 160
Status information and/or state data packets, in order to reclaim carrier status information play back.Information storage module 160
It is preferred that capacity can be used to be stored for 8GB FLASH.
Further, front end monitoring apparatus 10 also optimizes and included in the present embodiment：Image capture module 170, is fixedly arranged on
The recovery carrier surface, electrically connected by signal control interface with Central Control Module 130, for according to Central Control Module
130 control signals sent, start or stop and IMAQ carried out to the surrounding environment of the recovery carrier,
Wherein, the control signal receives the control instruction of the feedback of ground monitoring device 20 in Central Control Module 130
After generate；
Accordingly, ground monitoring device 20, it is additionally operable to send out by the forward end supervising device 10 of the second data transmission module 210
The control instruction for sending triggering to generate.
Specifically, signal control interface can be understood as controlling the signaling interface of image capture module 170.In the present embodiment
In, after the triggering generation control instruction of ground monitoring device 20, the control instruction is fed back by the second data transmission module 210
To front end monitoring apparatus 10.After first data transmission module 140 receives the control instruction in front end monitoring apparatus 10, by institute
State control instruction and feed back to Central Control Module 130.Central Control Module 130 can generate and be used for according to the control instruction
Control the control signal of image capture module 170.And feed back to the signal control interface of image capture module 170, with start or
Person stops carrying out IMAQ to the surrounding environment for reclaiming carrier.
Recovery carrier surrounding environment is carried out in image acquisition process it will be evident that working as image capture module 170, the figure of collection
As signal by signal transmission interface feeds back to Central Control Module 130.Central Control Module 130 will handle the picture number obtained
First data transmission module 140 is fed back to according to bag, described image packet is fed back into ground monitoring device 20.Ground monitoring
Device 20 can monitor the surrounding environment of recovery carrier in real time based on described image packet.In addition, image capture module 170 is adopted
The view data bag that picture signal and Central Control Module 130 processing of collection obtain can be stored in information storage module 160,
To realize the playback to reclaiming carrier ambient condition information.
Further, ground monitoring device 20 also optimizes and included in the present embodiment：First playback module 240, for
When receiving the first play-back command of triggering generation, the historic state of carrier is reclaimed described in ground monitoring device 20 to being stored in
Information and/or historical state data carry out information playback and shown.
Specifically, the first playback module 240 can be understood as the playback module to the storage information of ground monitoring device 20.The
One play-back command can be understood as the play-back command corresponding to the first playback module 240.
In the present embodiment, when triggering the first play-back command, the playback display of the first playback module 240 is stored in ground
The historic state information and/or historical state data of carrier are reclaimed described in supervising device 20.It is understood that ground is supervised
Control device 20 can store to the status information and/or state data packets monitored in real time, be shown with carrying out playback.
Further, ground monitoring device 20 also optimizes and included in the present embodiment：Second playback module 250, for
When receiving the second play-back command of triggering generation, second play-back command is fed back into front end monitoring apparatus with signal form
10, information playback is carried out to the historic state information and/or historical state data received and shown,
Wherein, historic state information and/or historical state data are stored in the information storage mould of front end monitoring apparatus 10
In block 160；
It is corresponding, front end monitoring apparatus 10, it is additionally operable to when receiving second play-back command, by information storage module
The historic state information and/or historical state data stored in 160 feeds back to ground monitoring device 20.
Specifically, the second playback module 250 can be understood as storing information storage module 160 in front end monitoring apparatus 10
The playback module of information.Second play-back command can be understood as the play-back command corresponding to the second playback module 250.
In the present embodiment, when triggering the second play-back command, ground monitoring device 20 is by second play-back command
Front end monitoring apparatus 10 is fed back to signal form.When front end monitoring apparatus 10 receives the second play-back command, information is stored
The historic state information and/or historical state data stored in module 160 feeds back to ground monitoring device 20.Ground monitoring fills
Put the 20 pairs of historic state received information and/or historical state data carries out information playback and shown.
The structural representation for another recovery monitoring system that the embodiment of the present invention three provides, optimization add information storage
Module, image capture module, the first playback module and the second playback module.Using the recovery monitoring system, information can be passed through
Memory module and the second playback module, can be to storing on the basis of to the monitoring in real time of recovery carrier in front end monitoring apparatus
Recovery carrier status information and/or state data packets played back, by the first playback module, ground monitoring can be filled
The status information and/or state data packets for putting the recovery carrier of middle storage are played back.Can be to recovery carrier in flight course
In status information and/or state data packets carry out more careful research and analysis, more accurately to find emission system
Need to improve the place upgraded.The ambient condition information of recovery carrier can be monitored in real time by image capture module, with more
The accurately status information in monitoring recovery carrier flight course, is easy to the real-time monitoring to reclaiming carrier.
Pay attention to, above are only presently preferred embodiments of the present invention and institute's application technology principle.It will be appreciated by those skilled in the art that
The invention is not restricted to specific embodiment described here, can carry out for a person skilled in the art various obvious changes,
Readjust and substitute without departing from protection scope of the present invention.Therefore, although being carried out by above example to the present invention
It is described in further detail, but the present invention is not limited only to above example, without departing from the inventive concept, also
Other more equivalent embodiments can be included, and the scope of the present invention is determined by scope of the appended claims.
Claims (10)
1. one kind recovery monitoring system, it is characterised in that including：Front end monitoring apparatus and ground monitoring device；
The front end monitoring apparatus, it is laid on recovery carrier, for monitoring the status information of recovery carrier, handles described in obtaining
The state data packets of carrier are reclaimed, and Real-time Feedback is to the ground monitoring device；
The ground monitoring device, is laid on ground control cabinet, for receiving the status number of the front end monitoring apparatus feedback
According to bag, to monitor the state of flight of the recovery carrier in real time based on the state data packets.
2. system according to claim 1, it is characterised in that the front end monitoring apparatus includes：Satellite navigation monitors mould
Block, Sensor monitoring module, Central Control Module, first data transmission module and the first power module；
The satellite navigation monitoring module, is electrically connected with the Central Control Module, monitors the virtual condition of the recovery carrier
Information, and feed back to the Central Control Module；
The Sensor monitoring module, is electrically connected with the Central Control Module, and the recovery carrier is arranged at for basis
Sensor monitoring obtain the second status information, and feed back to the Central Control Module；
The Central Control Module, electrically connected with the first data transmission module, for from the virtual condition information of reception
First state information is extracted, and first state information that synchronization receives and the second status information are merged into processing,
Obtain it is described recovery carrier the moment state data packets and feed back to the first data transmission module；
The first data transmission module, for the state data packets at the moment to be fed back into the ground monitoring device；
First power module, for for the satellite navigation monitoring module, Sensor monitoring module, Central Control Module with
And first data transmission module for power supply.
3. system according to claim 2, it is characterised in that the satellite navigation monitoring module, including：At least two letters
Number dual-mode antenna, combiner and signal receiver；
At least two signal transmitting and receivings antenna, with different positions and pose be fixedly arranged on it is described recovery carrier on, respectively with the combiner
Electrical connection, for receiving the signal data for the relevant recovery carrier that satellite navigation system is sent in different positions and pose, and feed back
To the combiner；
The combiner, electrically connected with the signal receiver, for the letter fed back at least two supported signal dual-mode antennas
Number carries out fusion treatment, obtains the actual signal data of the recovery carrier, and feeds back to the signal receiver；
The signal receiver, electrically connected with the Central Control Module, for determining institute according to the actual signal data of reception
The virtual condition information of recovery carrier is stated, and feeds back to the Central Control Module, wherein, the virtual condition information includes：
Position, Velocity and Time information.
4. system according to claim 2, it is characterised in that the Sensor monitoring module, including：Sensor monitoring connects
Mouth and pressure sensor, acceleration transducer and the temperature sensor for being fixedly arranged on the recovery carrier surface；
The Sensor monitoring interface, is electrically connected with the Central Control Module, for receiving the pressure sensor collection
The temperature information of pressure information, the acceleration information of acceleration transducer collection and temperature sensor collection, shape
Into the second status information for feeding back to the Central Control Module.
5. system according to claim 2, it is characterised in that the ground monitoring device includes：Second data transfer mould
Block, monitoring module and second source module；
Second data transmission module, is electrically connected with the monitoring module, for receiving the front end monitoring apparatus feedback
State data packets, and feed back to the monitoring module；
The monitoring module, for monitoring the state of flight of the recovery carrier in real time based on the state data packets；
The second source module, for being powered for second data transmission module.
6. system according to claim 5, it is characterised in that the first data transmission module is to include front end radio station
The front end data radio station of antenna, for by the state data packets in the form of data-signal it is anti-by the front end radio antenna
It is fed to the ground monitoring device；
Second data transmission module is the ground data radio station for including land station antenna, for passing through ground electricity
Platform antenna receives the data-signal of front end radio antenna feedback, obtains state data packets corresponding to the data-signal and anti-
It is fed to the monitoring module.
7. system according to claim 1, it is characterised in that the front end monitoring apparatus also includes：
Information storage module, for reclaiming the status information and state data packets of carrier described in real-time storage.
8. system according to claim 2, it is characterised in that the front end monitoring apparatus also includes：
Image capture module, the recovery carrier surface is fixedly arranged on, passes through signal control interface and Central Control Module electricity
Connection, for the control signal sent according to the Central Control Module, start or stop surrounding's ring to the recovery carrier
Border carries out IMAQ,
Wherein, the control signal is after the control instruction that the Central Control Module receives the ground monitoring device feedback
Generation；
Accordingly, the ground monitoring device, it is additionally operable to send to the front end monitoring apparatus by the second data transmission module
Trigger the control instruction of generation.
9. system according to claim 1, it is characterised in that the ground monitoring device also includes：
First playback module, for when receiving the first play-back command of triggering generation, being filled to being stored in the ground monitoring
The historic state information of carrier is reclaimed described in putting and/or historical state data carries out information playback and shown.
10. system according to claim 7, it is characterised in that the ground monitoring device also includes：
Second playback module, for when receiving the second play-back command of triggering generation, by second play-back command to believe
Number form feeds back to the front end monitoring apparatus, and letter is carried out to the historic state information and/or historical state data received
Breath playback display,
Wherein, historic state information and/or historical state data are stored in the information storage module of front end monitoring apparatus；
It is corresponding, the front end monitoring apparatus, it is additionally operable to, when receiving second play-back command, described information be stored into mould
The historic state information and/or historical state data stored in block feeds back to the ground monitoring device.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710947536.8A CN107728498A (en) | 2017-10-12 | 2017-10-12 | One kind recovery monitoring system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710947536.8A CN107728498A (en) | 2017-10-12 | 2017-10-12 | One kind recovery monitoring system |
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Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4924401A (en) * | 1987-10-30 | 1990-05-08 | The United States Of America As Represented By The Secretary Of The Air Force | Aircraft ground collision avoidance and autorecovery systems device |
| CN201004174Y (en) * | 2007-01-26 | 2008-01-09 | 青岛天骄无人机遥感技术有限公司 | Ground monitoring system for unmanned plane |
| CN101298974A (en) * | 2007-04-30 | 2008-11-05 | 凯迈(洛阳)电子有限公司 | Active recycling control method of air-to-air missile experiment missile |
| CN201266089Y (en) * | 2008-09-05 | 2009-07-01 | 北京七维航测科技发展有限公司 | INS/GPS combined navigation system |
| CN106034147A (en) * | 2015-03-16 | 2016-10-19 | 北京军懋国兴科技股份有限公司 | Multi-machine aircraft data real -time monitoring system |
| CN106646521A (en) * | 2016-12-20 | 2017-05-10 | 航天恒星科技有限公司 | Flying terminal recycling method and device |
| CN106970638A (en) * | 2017-03-09 | 2017-07-21 | 北京航天控制仪器研究所 | A kind of accurate air-drop monitoring dissemination system |
-
2017
- 2017-10-12 CN CN201710947536.8A patent/CN107728498A/en active Pending
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4924401A (en) * | 1987-10-30 | 1990-05-08 | The United States Of America As Represented By The Secretary Of The Air Force | Aircraft ground collision avoidance and autorecovery systems device |
| CN201004174Y (en) * | 2007-01-26 | 2008-01-09 | 青岛天骄无人机遥感技术有限公司 | Ground monitoring system for unmanned plane |
| CN101298974A (en) * | 2007-04-30 | 2008-11-05 | 凯迈(洛阳)电子有限公司 | Active recycling control method of air-to-air missile experiment missile |
| CN201266089Y (en) * | 2008-09-05 | 2009-07-01 | 北京七维航测科技发展有限公司 | INS/GPS combined navigation system |
| CN106034147A (en) * | 2015-03-16 | 2016-10-19 | 北京军懋国兴科技股份有限公司 | Multi-machine aircraft data real -time monitoring system |
| CN106646521A (en) * | 2016-12-20 | 2017-05-10 | 航天恒星科技有限公司 | Flying terminal recycling method and device |
| CN106970638A (en) * | 2017-03-09 | 2017-07-21 | 北京航天控制仪器研究所 | A kind of accurate air-drop monitoring dissemination system |
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