CN109949640A - A kind of winged training device of the extension of guided weapon system - Google Patents
A kind of winged training device of the extension of guided weapon system Download PDFInfo
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- 238000012549 training Methods 0.000 title claims abstract description 64
- 238000004146 energy storage Methods 0.000 claims abstract description 56
- 230000005669 field effect Effects 0.000 claims abstract description 45
- 238000004088 simulation Methods 0.000 claims abstract description 24
- 230000010365 information processing Effects 0.000 claims description 15
- 230000001052 transient effect Effects 0.000 claims description 13
- 239000003990 capacitor Substances 0.000 claims description 12
- 238000004891 communication Methods 0.000 claims description 12
- 230000000087 stabilizing effect Effects 0.000 claims description 9
- 238000003860 storage Methods 0.000 claims description 8
- 238000006243 chemical reaction Methods 0.000 claims description 7
- 238000001914 filtration Methods 0.000 claims description 6
- 238000012545 processing Methods 0.000 claims description 2
- 238000004519 manufacturing process Methods 0.000 abstract description 5
- 238000005265 energy consumption Methods 0.000 abstract description 2
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- 238000010586 diagram Methods 0.000 description 6
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- 238000013461 design Methods 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 238000006467 substitution reaction Methods 0.000 description 2
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- 238000005520 cutting process Methods 0.000 description 1
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Abstract
The extension that the present invention provides a kind of guided weapon system flies training device, it hangs the outer dimension, quality center of mass, rotary inertia, electrical load and the workflow that fly training device and Real Rocket is consistent, alternative Real Rocket training shooter shoots and unloads bullet, it can also substitute whether live shell verifying rocket matches with the electric interfaces of carrier aircraft system, significantly reduce production cost and experimentation cost, weapon system trainer demand can be met with higher compatible degree, improve weapon system trainer efficiency and fighting capacity；In addition, the present invention using the normally closed operational characteristic of field-effect tube to the in-orbit state simulation that leaves the right or normal track of rocket, production cost, service life and the reliability hung and fly training device greatly improved；Meanwhile the problems such as field-effect tube has the features such as low in energy consumption, long service life due to its operational characteristic, and energy-storage module is complicated greatly caused by having broken traditional relay simulation opened/closed bring restricted lifetime and power consumption greatly.
Description
Technical field
The invention belongs to the extensions of airborne guided weapon to fly training technique field more particularly to a kind of extension of guided weapon system
Fly training device.
Background technique
To promote shooter's skilled operation degree and weapon system fighting capacity, shooter and weapon system need to be drilled repeatedly.
Currently, common practice both domestic and external is, simulated maneuver is carried out using analogue system, this method can not real simulation weapon system work
The environmental condition in wartime, or leave the right or normal track using the relay mode simulated rocket that physics interlocks is in-orbit, this method significantly reduces extension
Fly the service life of dummy round.And flown using Real Rocket extension expensive, and hang and fly restricted lifetime, brings many maintenances and folding
Old equal military expenditures.
Summary of the invention
To solve the above problems, the present invention provide a kind of guided weapon system extension fly training device, for shooter training and
Weapon system rehearsal provides a set of real simulation rocket configuration size, quality center of mass, rotary inertia, electrical load and workflow
The extension of journey flies dummy round, meets weapon system trainer demand with higher compatible degree at lower cost, improves weapon system
Training effectiveness and fighting capacity.
A kind of winged training device of the extension of guided weapon system, is mounted on carrier aircraft system, including simulation bay section, is mounted on simulation
Simulation empennage outside bay section and the power control board, information processing board and fictitious load for being mounted on boiler-plate intersegmental part
Plate, wherein simulation bay section and outer dimension, the quality, mass center for simulating simulated rocket and Real Rocket to be simulated that empennage is constituted
And rotary inertia is all the same；
The power control board includes A D interface module, the first energy-storage module, power management module and field-effect pipe die
Block；The information processing board includes that AD acquisition module, processor module, the first discrete magnitude output module and the second discrete magnitude are defeated
Module out；
The carrier aircraft system is used to export mould for power management module, AD acquisition module, processor module, the first discrete magnitude
Block and the power supply of the second discrete magnitude output module；
The A D interface module is used to receive the transmitting hard signal that the carrier aircraft system provides, and by the transmitting rigid line
Signal is transmitted to the processor module by AD acquisition module；
Whether the voltage that the processor module is used to detect transmitting hard signal is greater than preset threshold, if more than then controlling
It makes the first discrete magnitude output module to power to the first energy-storage module, then the first energy-storage module driving FET module is disconnected
It opens；If being not more than, the first discrete magnitude output module is not powered to the first energy-storage module, and field-effect tube module remains closed；
Processor module is also used to the working sequence according to preset Real Rocket to be simulated, and controls the second discrete magnitude output module to electricity
Source control module exports power supply signal；
The power management module is used for when receiving power supply signal, provides working power for fictitious load plate, otherwise
Working power is not provided to fictitious load plate；
The fictitious load plate is identical as the true electrical load of Real Rocket to be simulated, and with power supply pipe parallel with one another
Reason module and the first energy-storage module are all connected with, for simulating under different operating conditions the transient working electric current of Real Rocket to be simulated and steady
State operating current；
The field-effect tube module is connected in the in-orbit closed circuit that leaves the right or normal track of carrier aircraft system, is used for Hang flight simulation training cartridge
It set in-orbit and leaves the right or normal track；Wherein, when field-effect tube disconnects, the in-orbit closed circuit disconnection that leaves the right or normal track hangs winged training device and leaves the right or normal track；Field effect
Should pipe closure when, it is in-orbit leave the right or normal track closed circuit closure, hang fly training device it is in-orbit；
First energy-storage module is used to make field-effect tube keep disconnected within the set duration when the field-effect tube disconnects
Open state, meanwhile, the power supply of fictitious load plate is continued as in the setting duration；It is also used to release when the energy of itself storage
Bi Hou is closed field-effect tube, and it is again automatic in-orbit to hang winged training device.
Further, the fictitious load plate includes capacitor, inductance and power resistor；Wherein, capacitor, inductance and function
Rate resistance is identical as the true electrical load of Real Rocket to be simulated, and is connected on phase with inductance after capacitor and power resistor parallel connection
The mutually both ends of power management module in parallel and the first energy-storage module.
Further, the power control board further includes filter module；
The filter module is used to for the supply voltage that the carrier aircraft system provides being filtered and pressure stabilizing, by filtering and
Supply voltage after pressure stabilizing be again power management module, AD acquisition module, processor module, the first discrete magnitude output module and
The power supply of second discrete magnitude output module.
Further, the information processing board further includes DC/DC conversion module；
The DC/DC conversion module will convert into for converting to the supply voltage after filtering and pressure stabilizing
The supply voltage of setting value is exported to AD acquisition module, processor module, the first discrete magnitude output module and the second discrete magnitude
Module provides working power.
Further, the information processing board further includes communication module；
The communication module is used for the transient working electric current and steady state operating current of fictitious load plate, field-effect tube module
Working condition and the working condition of the first energy-storage module be sent to carrier aircraft system；It is also used to receive the pre- of carrier aircraft system offer
If Real Rocket to be simulated working sequence, the working sequence of preset Real Rocket to be simulated then is transmitted to the place
Manage device module.
Further, a kind of extension of guided weapon system flies training device, further includes logger；The logger includes letter
Number acquisition module, single-chip microcontroller and FLASH module；
The signal acquisition module is for acquiring and forwarding the communication module to send to carrier aircraft system to the single-chip microcontroller
Fictitious load plate transient working electric current and steady state operating current, the working condition of field-effect tube module and the first energy storage mould
The working condition of block；
The single-chip microcontroller is used to control the read-write of FLASH module, make its record the transient working electric current of fictitious load plate and
The working condition of steady state operating current, field-effect tube module working condition and the first energy-storage module.
Further, a kind of extension of guided weapon system flies training device, further includes the second energy-storage module；
The electric energy of the second energy-storage module storage is provided by carrier aircraft system, for working as the supply voltage hit of carrier aircraft system
When, it is power management module, AD acquisition module, processor module, the first discrete magnitude output module and the output of the second discrete magnitude
Module for power supply.
The utility model has the advantages that
1, the extension that the present invention provides a kind of guided weapon system flies training device, hangs outer dimension, the matter for flying training device
Amount mass center, rotary inertia, electrical load and workflow and Real Rocket are consistent, alternative Real Rocket training shooter
Bullet is shot and unloaded, can also substitute whether live shell verifying rocket matches with the electric interfaces of carrier aircraft system, significantly reduces production
Cost and experimentation cost can meet weapon system trainer demand with higher compatible degree, improve weapon system trainer effect
Rate and fighting capacity；
In addition, the present invention using the normally closed operational characteristic of field-effect tube to the in-orbit state simulation that leaves the right or normal track of rocket, substantially
Improve production cost, service life and the reliability hung and fly training device；Meanwhile field-effect tube is due to its operational characteristic, tool
There is the features such as low in energy consumption, long service life, has broken traditional relay simulation opened/closed bring restricted lifetime and power consumption is big
The problems such as caused big energy-storage module is complicated, simplifies design logic, reduces production cost, improve product reliability and
Service life, filled up at home and abroad left the right or normal track in the market using normally closed field-effect tube substitution relay simulated rocket at present/
The blank of rail；
It can be seen that compared to general weapon system simulation training technique, the present invention can comprehensive simulated live shell, and not
Being flown the service life by use environment and hanging is influenced, can multiple the leaving the right or normal track of automatic imitation rocket/in-orbit, it is quasi- with inexpensive high precision feature
True simulated rocket structure, electrical characteristic and workflow.
2, the extension that the present invention provides a kind of guided weapon system flies training device, passes through capacitor, inductance and power resistor mould
Field trial cost, the electricity of substitution Real Rocket verifying and carrier aircraft system can be greatly reduced in the quasi- true electrical load of rocket
It is true by capacitor, inductance and power resistor simulated rocket to have filled up the winged training device field of current extension for gas Interface Matching
The blank of electrical load.
Detailed description of the invention
Fig. 1 is that a kind of extension of guided weapon system provided by the invention flies the structural schematic diagram of training device；
Fig. 2 is the structural schematic diagram of power control board provided by the invention；
Fig. 3 is the connection relationship signal of fictitious load plate provided by the invention and power management module and the first energy-storage module
Figure；
Fig. 4 is the operation principle schematic diagram of information processing board provided by the invention.
Specific embodiment
In order to make those skilled in the art more fully understand application scheme, below in conjunction in the embodiment of the present application
Attached drawing, the technical scheme in the embodiment of the application is clearly and completely described.
Referring to Fig. 1, which is that a kind of extension of guided weapon system provided in this embodiment flies the structural representation of training device
Figure.A kind of winged training device of the extension of guided weapon system, is mounted on carrier aircraft system, including simulation bay section, is mounted on simulation bay section
The simulation empennage of outside and power control board, information processing board, fictitious load plate and the note for being mounted on boiler-plate intersegmental part
Record device, wherein simulation bay section and outer dimension, quality, mass center and the rotary inertia for simulating empennage and Real Rocket to be simulated
It is all the same.
It should be noted that hanging the power control board for flying training device by simulating electric interfaces and carrier aircraft system in bay section
System is connected, and carrier aircraft system provides working power all the way and transmitting hard signal to winged training device is hung by electric interfaces, and real
When bind set of data information, hang and fly training device and report itself job information to carrier aircraft system in real time by electric interfaces, with this
Realize that Real Rocket to be simulated and carrier aircraft system carry out the process of information exchange.
Optionally, the simulation bay section and simulation empennage are using socket or thread connecting mode, at power control board, information
Reason plate and fictitious load plate are mounted on circuit board support by screw, and circuit board support and logger are fixed by screws in mould
In quasi- bay section.
Referring to fig. 2, which is the structural schematic diagram of power control board provided in this embodiment.The power control board includes
Filter module, A D interface module, the first energy-storage module, the second energy-storage module, power management module and field-effect tube module；Institute
Stating information processing board includes communication module, AD acquisition module, DC/DC conversion module, processor module, the first discrete magnitude output mould
Block and the second discrete magnitude output module；The fictitious load plate includes capacitor, inductance and power resistor；Wherein, referring to figure
3, which is the connection relationship diagram of fictitious load plate and power management module and the first energy-storage module provided in this embodiment.
Capacitor, inductance and power resistor are identical as the true electrical load of Real Rocket to be simulated, and capacitor and power resistor are in parallel
The both ends for being connected to power management module and the first energy-storage module parallel with one another are connected on inductance afterwards, for simulating different works
The transient working electric current and steady state operating current of Real Rocket to be simulated under condition.Wherein, capacitor and inductance are for simulated rocket
Transient working electric current, power resistor are used for the steady state operating current of simulated rocket.The logger includes signal acquisition module, list
Piece machine and FLASH module.
It should be noted that general straight cutting Chip-R cannot all expire since fictitious load electric current is larger, power consumption is larger
Foot requires, therefore the present embodiment is using the power resistor for meeting power consumption requirements.
The filter module is used to for the supply voltage that the carrier aircraft system provides being filtered and pressure stabilizing, by filtering and
Supply voltage after pressure stabilizing is power management module, the power supply of the second energy-storage module again.Filter module is designed as hanging winged training cartridge
It sets and provides good electromagnetic environment, ensure that the Electro Magnetic Compatibility and reliability hung and fly training device.
The DC/DC conversion module will convert into for converting to the supply voltage after filtering and pressure stabilizing
The supply voltage of setting value is communication module, AD acquisition module, processor module, the first discrete magnitude output module and second again
The power supply of discrete magnitude output module.
Optionally, DC/DC conversion module is made of MJWI10-24S05.
The A D interface module is used to receive the transmitting hard signal that the carrier aircraft system provides, and by the transmission rigid line
Signal is transmitted to the processor module by AD acquisition module.
Optionally, AD acquisition module is made of ADUM3190, is connected with the A D interface module of power control board, for acquiring
Emit hard signal.
Whether the voltage that the processor module is used to detect transmitting hard signal is greater than preset threshold, if more than then controlling
It makes the first discrete magnitude output module to power to the first energy-storage module, then the first energy-storage module driving FET module is disconnected
It opens；If being not more than, the first discrete magnitude output module is not powered to the first energy-storage module, and field-effect tube module remains closed；
Processor module is also used to the working sequence according to preset Real Rocket to be simulated, and controls the second discrete magnitude output module to electricity
Source control module exports power supply signal.
Optionally, processor module is made of TMS320LF2403A.
The power management module is used for when receiving power supply signal, provides working power for fictitious load plate, otherwise
Working power is not provided to fictitious load plate.
Optionally, the first discrete magnitude output module is made of with the second discrete magnitude output module MC1413, by processor mould
The control of block makes the first energy-storage module driving FET module open or close for offer and keeps power management module defeated
Out or the power supply signal of disconnection power supply, the power supply signal are high level or low level.
The field-effect tube module is connected in the in-orbit closed circuit that leaves the right or normal track of carrier aircraft system, is used for Hang flight simulation training cartridge
It set in-orbit and leaves the right or normal track；Wherein, when field-effect tube disconnects, the in-orbit closed circuit disconnection that leaves the right or normal track hangs winged training device and leaves the right or normal track；Field effect
Should pipe closure when, it is in-orbit leave the right or normal track closed circuit closure, hang fly training device it is in-orbit.
First energy-storage module is used to make field-effect tube keep disconnected within the set duration when the field-effect tube disconnects
Open state, meanwhile, the power supply of fictitious load plate is continued as in the setting duration；It is also used to release when the energy of itself storage
Bi Hou is closed field-effect tube, and it is again automatic in-orbit to hang winged training device.
It should be noted that when carrier aircraft system acquisition is to the moment for flying training device and leaving the right or normal track is hung training device can be flown to hanging
Power-off, hanging winged training device needs to keep the signal that leaves the right or normal track at least 1s under power blackout situation, and carrier aircraft system, which determines to hang accordingly, flies training
Device whether successful launch.I.e. field-effect tube keeps itself opening state according to the energy of the first energy-storage module, when
The release of one energy-storage module energy finishes, and field-effect tube restores closed state, i.e. the winged training device of extension is in-orbit, to emit next time
Process.
The electric energy of the second energy-storage module storage is provided by carrier aircraft system, for working as the supply voltage hit of carrier aircraft system
When, it is power management module, AD acquisition module, processor module, the first discrete magnitude output module and the output of the second discrete magnitude
Module for power supply.The design of second energy-storage module ensure that the anti-power down hung and fly training device.
It should be noted that the first energy-storage module is connected between the grid of field-effect tube and source electrode, when grid and source electrode electricity
When pressure is greater than threshold voltage, field-effect tube is disconnected.Second energy-storage module is to connect at the very start in charging with field-effect tube
First energy-storage module just charges when being the first discrete magnitude output module output high level.That is, when the first discrete output
When module provides high level, first the first energy-storage module is set to charge to the power supply of the first energy-storage module, the first energy-storage module driving field again
Effect pipe disconnects, after field-effect tube disconnects, carrier aircraft system cut-off, then it is a little while electric by the first energy-storage module confession, to the letter that leaves the right or normal track
It number is kept.
The communication module is used for the transient working electric current and steady state operating current of fictitious load plate, field-effect tube module
Working condition, the working condition of the working condition of the first energy-storage module and the second energy-storage module be sent to carrier aircraft system；Also
For receiving the working sequence of the preset Real Rocket to be simulated of carrier aircraft system offer, then by preset wait simulate true fire
The working sequence of arrow is transmitted to the processor module.
It should be noted that the communication module of information processing board is made of MAX3490, information exchange is carried out with carrier aircraft system
Connection cross line from power control board after, be connected by electric interfaces with carrier aircraft system.Communication module is by sending height electricity
It is flat to hang the signal reportings carrier aircraft systems such as working condition, the voltage and current for flying training device, it is executed by receiving low and high level
The instruction of carrier aircraft system control process and all metamessages of bookbinding.
Referring to fig. 4, which is the operation principle schematic diagram of information processing board provided in this embodiment.The signal acquisition mould
The transient working of fictitious load plate of the block for acquiring and forwarding the communication module to send to carrier aircraft system to the single-chip microcontroller
The working condition of electric current and steady state operating current, the working condition of field-effect tube module and the first energy-storage module；
The single-chip microcontroller is used to control the read-write of FLASH module, make its record the transient working electric current of fictitious load plate and
The working condition of steady state operating current, field-effect tube module working condition and the first energy-storage module.
Optionally, single-chip microcontroller is made of STM32, and FLASH module is made of the NAND FLASH of 256Gbit, signal acquisition
Module is made of ADS7950.
The extension of the present embodiment flies the course of work of training device are as follows:
After the completion of the winged training device of extension is shot, carrier aircraft powers on hanging point, hangs winged training device and works with carrier aircraft system
Process and information exchange, carrier aircraft system provide working power and bookbinding Chu's metamessage to winged training device is hung, and hang winged training device
Power control board power supply is filtered and energy storage mentions the power supply after energy storage when the supply voltage hit of carrier aircraft system
Supply information processing board and logger, and mentioned power supply according to the low and high level of the second discrete magnitude output module of information processing board
Supply fictitious load plate.Whether AD acquisition module assigns transmitting hard signal with the period real-time query carrier aircraft system of 1ms, processing
Whether device module is greater than preset threshold according to the voltage of the collected transmitting hard signal of AD acquisition module, controls the first discrete magnitude
Output module exports low and high level, if powers to the first energy-storage module, so that the first energy-storage module of control whether imitate by driving field
It answers tube module to open, makes the in-orbit closed circuit disconnection that leaves the right or normal track being connected with carrier aircraft system, hang winged training device and leave the right or normal track, to realize
Rocket leaves the right or normal track simulation, and the state that leaves the right or normal track that the first energy-storage module carries out at least 1s to the signal that leaves the right or normal track is kept, and guarantees that carrier aircraft judgement is hung and flies
Training device transmitting is normal, and leave the right or normal track success, after the first energy-storage module energy discharges, due to the operational characteristic of field-effect tube,
Be closed again, be connected with carrier aircraft it is in-orbit leave the right or normal track to form closed circuit, hang fly training device it is automatically in-orbit, can carry on next
Secondary transmitting process.Logger binds Chu Yuanxin to the analog signal, digital signal and carrier aircraft for flying training device is hung in whole process
Breath is stored, and downloads back read data by USB port.
Certainly, the invention may also have other embodiments, without deviating from the spirit and substance of the present invention, ripe
Various corresponding changes and modifications can be made according to the present invention certainly by knowing those skilled in the art, but these it is corresponding change and
Deformation all should fall within the scope of protection of the appended claims of the present invention.
Claims (7)
1. a kind of extension of guided weapon system flies training device, it is mounted on carrier aircraft system, which is characterized in that including simulating bay section,
The simulation empennage that is mounted on outside simulation bay section and be mounted on the power control board of boiler-plate intersegmental part, information processing board and
Fictitious load plate, wherein simulation bay section and outer dimension, the matter for simulating simulated rocket and Real Rocket to be simulated that empennage is constituted
Amount, mass center and rotary inertia are all the same；
The power control board includes A D interface module, the first energy-storage module, power management module and field-effect tube module；Institute
Stating information processing board includes AD acquisition module, processor module, the first discrete magnitude output module and the second discrete magnitude output mould
Block；
The carrier aircraft system be used for for power management module, AD acquisition module, processor module, the first discrete magnitude output module with
And second discrete magnitude output module power supply；
The A D interface module is used to receive the transmitting hard signal that the carrier aircraft system provides, and by the transmitting hard signal
The processor module is transmitted to by AD acquisition module；
Whether the voltage that the processor module is used to detect transmitting hard signal is greater than preset threshold, if more than institute is then controlled
It states the first discrete magnitude output module to power to the first energy-storage module, then the first energy-storage module driving FET module disconnects；
If being not more than, the first discrete magnitude output module is not powered to the first energy-storage module, and field-effect tube module remains closed；Processing
Device module is also used to the working sequence according to preset Real Rocket to be simulated, and controls the second discrete magnitude output module to power supply pipe
It manages module and exports power supply signal；
The power management module be used for when receiving power supply signal, provide working power for fictitious load plate, otherwise not to
Fictitious load plate provides working power；
The fictitious load plate is identical as the true electrical load of Real Rocket to be simulated, and with power management mould parallel with one another
Block and the first energy-storage module are all connected with, for simulating the transient working electric current and stable state work of Real Rocket to be simulated under different operating conditions
Make electric current；
The field-effect tube module is connected in the in-orbit closed circuit that leaves the right or normal track of carrier aircraft system, for Hang flight simulation training device
It is in-orbit and leave the right or normal track；Wherein, when field-effect tube disconnects, the in-orbit closed circuit disconnection that leaves the right or normal track hangs winged training device and leaves the right or normal track；Field-effect tube
When closure, it is in-orbit to hang winged training device for the in-orbit closed circuit closure that leaves the right or normal track；
First energy-storage module is used to make field-effect tube remain open shape within the set duration when the field-effect tube disconnects
State, meanwhile, the power supply of fictitious load plate is continued as in the setting duration；It is also used to finish when the energy release of itself storage
Afterwards, it is closed field-effect tube, it is again automatic in-orbit hangs winged training device.
2. a kind of extension of guided weapon system as described in claim 1 flies training device, which is characterized in that the fictitious load
Plate includes capacitor, inductance and power resistor；Wherein, capacitor, inductance and power resistor and Real Rocket to be simulated is true
Electrical load is identical, and is connected on power management module and the first storage parallel with one another after capacitor and power resistor parallel connection with inductance
The both ends of energy module.
3. a kind of extension of guided weapon system as described in claim 1 flies training device, which is characterized in that the power supply control
Plate further includes filter module；
The filter module is used to for the supply voltage that the carrier aircraft system provides being filtered and pressure stabilizing, by filtering and pressure stabilizing
Supply voltage afterwards is power management module, AD acquisition module, processor module, the first discrete magnitude output module and second again
The power supply of discrete magnitude output module.
4. a kind of extension of guided weapon system as claimed in claim 3 flies training device, which is characterized in that the information processing
Plate further includes DC/DC conversion module；
The DC/DC conversion module will convert into setting for converting to the supply voltage after filtering and pressure stabilizing
The supply voltage of value is to AD acquisition module, processor module, the first discrete magnitude output module and the second discrete magnitude output module
Working power is provided.
5. a kind of extension of guided weapon system as described in claim 1 flies training device, which is characterized in that the information processing
Plate further includes communication module；
The communication module is used for the work of the transient working electric current and steady state operating current of fictitious load plate, field-effect tube module
The working condition for making state and the first energy-storage module is sent to carrier aircraft system；It is also used to receive the preset of carrier aircraft system offer
Then the working sequence of preset Real Rocket to be simulated is transmitted to the processor by the working sequence of Real Rocket to be simulated
Module.
6. a kind of extension of guided weapon system as claimed in claim 5 flies training device, which is characterized in that further include record
Device；The logger includes signal acquisition module, single-chip microcontroller and FLASH module；
The signal acquisition module is used for the mould for acquiring and forwarding the communication module to send to carrier aircraft system to the single-chip microcontroller
The transient working electric current of quasi- load board and steady state operating current, the working condition of field-effect tube module and the first energy-storage module
Working condition；
The single-chip microcontroller is used to control the read-write of FLASH module, it is made to record the transient working electric current and stable state of fictitious load plate
The working condition of operating current, field-effect tube module working condition and the first energy-storage module.
7. a kind of extension of guided weapon system as described in claim 1 flies training device, which is characterized in that further include the second storage
It can module；
The electric energy of second energy-storage module storage is provided by carrier aircraft system, for when the supply voltage hit of carrier aircraft system,
For power management module, AD acquisition module, processor module, the first discrete magnitude output module and the second discrete magnitude output module
Power supply.
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| CN201910093023.4A CN109949640B (en) | 2019-01-30 | 2019-01-30 | Hanging and flying training device of guided weapon system |
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| KR20180070131A (en) * | 2016-12-16 | 2018-06-26 | 주식회사 한화 | Apparatus and method for simulation trainning for guidance weapons |
| CN108460469A (en) * | 2018-02-09 | 2018-08-28 | 许新群 | Guided aircraft ammunition electronic record automatic collection, analysis and management method and system |
| CN109253666A (en) * | 2018-09-07 | 2019-01-22 | 陕西中天火箭技术股份有限公司 | A kind of low cost simulated training rocket |
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| KR20180070131A (en) * | 2016-12-16 | 2018-06-26 | 주식회사 한화 | Apparatus and method for simulation trainning for guidance weapons |
| CN107797483A (en) * | 2017-09-11 | 2018-03-13 | 凯迈（洛阳）测控有限公司 | It is a kind of to hang the electronic building brick and mock-up release method for flying dummy round |
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| CN109253666A (en) * | 2018-09-07 | 2019-01-22 | 陕西中天火箭技术股份有限公司 | A kind of low cost simulated training rocket |
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| CN109949640B (en) | 2024-02-23 |
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