CN207488769U - Indicator of trapped personnel information collection aircraft - Google Patents
Indicator of trapped personnel information collection aircraft Download PDFInfo
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- CN207488769U CN207488769U CN201721747808.1U CN201721747808U CN207488769U CN 207488769 U CN207488769 U CN 207488769U CN 201721747808 U CN201721747808 U CN 201721747808U CN 207488769 U CN207488769 U CN 207488769U
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- module
- indicator
- trapped personnel
- information collection
- personnel information
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Abstract
The utility model is related to a kind of indicator of trapped personnel information collection aircraft, including aircraft skin, hollow-cup motor module, motor drive module and ultrasonic distance measuring module are provided on the aircraft skin, the aircraft skin is internally provided with STM32 one-chip computer modules, sound acquisition module, voice synthetic module, sound identification module, satellite positioning module, communication module, nine axis movement sensor modules, power module and clock module.The utility model combining wireless senses network technology and sound treatment technology, cycle in time is rescued using the gold that rescue personnel can not arrive at, the automatic information collection for carrying out indicator of trapped personnel and health estimation work, enter disaster-stricken scene for later rescue personnel and related data is provided, so as to make up the deficiency of current existing auxiliary rescue system, rescue efficiency is improved to the maximum extent, reduces the death rate of indicator of trapped personnel, avoids the generation of more domestic tragedies.
Description
Technical field
The utility model is related to a kind of data acquisition aircraft, in particular to a kind of indicator of trapped personnel information collection aircraft.
Background technology
The great natures such as earthquake, dangerous material explosion or Accidents Disasters have become one of China's citizen's major causes of death, sternly
Threaten the safety of people's life and property again.In the dead of these great natures or Accidents Disasters, larger portion
Point the dead is that building pressure of being caved in is pounded and cannot be rescued in time, for a long time the reasons such as asphyxia, excessive blood loss and lead
It is lethal to die.
Rescue personnel mainly detects indicator of trapped personnel under the building that caves in using following two methods and implements to rescue at present.One
Kind is using the life-detection instruments such as infrared, sound wave, radar detection sign of life, carries out life rescue.Another kind uses rescuing machine
Device people searches for locating trapped personnel, substitutes the work of danger zone rescue personnel, ensures the life security of rescue workers.Such as sky
Devastated image transmitting to rescue command center, ruins surface search robot are entered danger by middle rotor searching rescue machine people
Locating trapped personnel is searched in the building of danger, small gaps searching machine people pierces the rescue unapproachable fine gap of team member, subtracts
The dead angle of few searching rescue.But aerial rotor searching rescue machine people only transmits image data, does not acquire indicator of trapped personnel
Information and healthy estimation function.Life-detection instrument, ruins surface search robot and small gaps searching machine people need to rescue
Personnel reach scene and are operated.When traffic is obstructed, (such as aftershock is constantly, there are toxic for shortage of manpower, rescue site bad environments
Gas) when reasons cause rescue personnel that can not carry these equipment arrival devastated at the first time, these equipment just can not
It plays a role.Meanwhile these equipment do not have network savvy, rescue personnel can not grasp the letter of the indicator of trapped personnel of entire devastated
Breath.
Utility model content
The utility model provides a kind of indicator of trapped personnel information collection aircraft, of the prior art its object is to overcome
Defect finds indicator of trapped personnel by sound acquisition module and sound identification module, communicated by communication module with outside and
When obtain indicator of trapped personnel information.
To achieve these goals, the utility model has following form：
The indicator of trapped personnel information collection aircraft, including aircraft skin, drag cup is provided on the aircraft skin
Motor module, motor drive module and ultrasonic distance measuring module, the aircraft skin are internally provided with STM32 microcontroller moulds
Block, sound acquisition module, voice synthetic module, sound identification module, satellite positioning module, communication module, nine axis motion-sensings
Device module, power module and clock module；
The motor drive module is connected with the hollow-cup motor module, and the power module is respectively the motor
Drive module, ultrasonic distance measuring module, STM32 one-chip computer modules, sound acquisition module, voice synthetic module, speech recognition mould
Block, satellite positioning module, communication module, nine axis movement sensor modules and clock module power supply, the STM32 one-chip computer modules
Respectively with the motor drive module, ultrasonic distance measuring module, sound acquisition module, voice synthetic module, sound identification module,
Satellite positioning module, communication module, nine axis movement sensor modules are connected with clock module.
Optionally, the hollow-cup motor module is four, and the hollow-cup motor module is respectively arranged at aircraft
Four wings；The ultrasonic distance measuring module is four, and the ultrasonic distance measuring module is respectively arranged at the side of the aircraft skin
Face.
Optionally, the STM32 one-chip computer modules use STM32F103C8 chips.
Optionally, the motor drive module uses 2SD315AI IGBT driving boards.
Optionally, the nine axis movement sensors module uses JY-901 modules.
Optionally, the sound acquisition module uses ATK-VS1053MP3 modules.
Optionally, the voice synthetic module uses XFS5152 chips.
Optionally, the sound identification module uses LD3320 chips.
Optionally, the communication module is ZigBee module, and the ZigBee module uses CC2530 chips.
Employ the indicator of trapped personnel information collection aircraft in the utility model, the autonomous flight in major disaster region,
By voice recognition and synthetic technology, the calling for help language of indicator of trapped personnel is identified, with indicator of trapped personnel human-computer dialogue, collect indicator of trapped personnel
Information；After the covering for completing monitoring region perceives, communicated, sent certainly with data collection facility using sensor network technology
The indicator of trapped personnel data of body acquisition；This programme combining wireless senses network technology and sound treatment technology, can not using rescue personnel
The gold rescue cycle in time of arrival, the automatic information collection for carrying out indicator of trapped personnel and health estimation work, are later rescue personnel
Related data is provided into disaster-stricken scene, so as to make up the deficiency of current existing auxiliary rescue system, improves rescue to the maximum extent
Efficiency is helped, reduces the death rate of indicator of trapped personnel, avoids the generation of more domestic tragedies.
Description of the drawings
Fig. 1 is the external structure block diagram of the indicator of trapped personnel information collection aircraft of the utility model；
Fig. 2 is the internal structure block diagram of the indicator of trapped personnel information collection aircraft of the utility model；
Fig. 3 is the structural principle block diagram of the indicator of trapped personnel information collection aircraft of the utility model.
Reference numeral：1- hollow-cup motor modules, 2- drive modules, 3-STM32 one-chip computer modules, 4- ultrasonic ranging moulds
Block, 5- aircraft skins, 6- sound acquisition modules, 7- voice synthetic modules, 8- sound identification modules, 9- satellite positioning modules,
10-ZigBee modules, nine axis movement sensor modules of 11-, 12- power modules, 13- clock modules.
Specific embodiment
In order to more clearly describe the technology contents of the utility model, come with reference to specific embodiment into traveling one
The description of step.
As shown in Figures 1 to 3, the utility model provides a kind of indicator of trapped personnel information collection aircraft, including aircraft outside
Shell 5, aircraft skin 5 are equipped with the hollow-cup motor module 1 for driving aircraft flight, the driving mould for driving motor
Block 2, the ultrasonic distance measuring module 4 for measuring aircraft and obstacle distance, aircraft skin 5 is interior to be equipped with to control flight
The STM32 one-chip computer modules 3 of device, for acquire search coverage sound sound acquisition module 6, for synthesize voice with by oppressive
The voice synthetic module 7 of member's exchange, for identifying the sound identification module 8 of indicator of trapped personnel voice, for locating trapped personnel
Manage position satellite positioning module 9, for send location information ZigBee module 10, for nine axis of heading to be controlled to transport
Move sensor assembly 11, for the power module 12 of power supply and for exporting the clock module 13 at current time.
In said program, power module 12 uses 12V rechargeable lithium batteries, can be with drive module 2, STM32 microcontrollers
Module 3, ultrasonic distance measuring module 4, sound acquisition module 6, voice synthetic module 7, sound identification module 8, satellite positioning module
9th, ZigBee module 10, nine axis movement sensors 11 and clock module 13 are connected, and provide 12V and 5V two kinds of different voltages, real
The power supply of existing module.
4 quantity of ultrasonic distance measuring module is 4 and is placed in aircraft fuselage surrounding.The hollow-cup motor module
1 quantity is 4 and is placed in aircraft rotary wings lower position.The drive module 2 is placed in aircraft parking stand position.It is described
STM32 one-chip computer modules 3, sound acquisition module 6, voice synthetic module 7, sound identification module 8, satellite positioning module 9,
ZigBee module 10, nine axis movement sensor modules 11, power module 12 and clock module 13 are mounted in aircraft skin.
The STM32 one-chip computer modules 3 use STM32F103C8 chips.STM32F103C8 singlechip microcontroller bands
There are one Embedded ARM cores, the built-in up to embedded Flash of 512KB, and available for storage program and data, 3 kinds of support is low
Power consumption mode.With 12 channel DMA controllers, the A/D converter of the us grades of 3 12,2 Channel 12-Bit D/A converters are applicable in
In motor control and strong jamming occasion.
The drive module 2 uses 2SD315AI IGBT driving boards.2SD315AI IGBT driving boards are integrated with intelligent drive
The functions such as dynamic, self-test, feedback of status, DC/DC power supplys, and control section is completely isolated with power section.The module uses arteries and veins
Transformer isolation mode is rushed, two-way IGBT drive signals can be generated simultaneously, it is possible to provide the peak of the driving voltage of ± 15V and ± 15A
It is worth electric current, there is accurately and reliably driving function and flexible adjustable overcurrent protection function, while supply voltage can be owed
Pressure detection, working frequency is up to more than 100kHz；Electrical isolation can reach 4000V AC.2SD315AI IGBT driving boards can spirit
It is living to define logic level, can unrestricted choice operating mode, there is short circuit and overcurrent protection function, there is under-voltage monitoring function, can
Dynamic setting short-circuit protection threshold value.
The satellite positioning module 9 uses ATK-S1216F8-BD GPS/ big dipper modules.ATK-S1216F8-BD GPS/
Big dipper module is a high-performance GPS/ big dipper modules of ALIENTEK productions, and module core is using SkyTraq companies
S1216F8-BD modules, have 167 channels, and tracking high sensitivity measures output frequency and reach as high as 20Hz up to -165dBm.
ATK-S1216F8-BD GPS/ modules use S1216F8-BD modules, and compact is had excellent performance.Module carries IPX interface,
Various active antennas can be connected, it is adaptable.
The ultrasonic distance measuring module 4 uses HC-SR04 chips, and HC-SR04 chips exemplary operation is 5V with voltage.It is extra small
Static working current is less than 2mA, and sensing angle is no more than 15 degree, and detection range reaches 2cm-400cm, and precision is up to 0.3cm, blind area
(2cm) is super near, triggers ranging.
The nine axis movement sensors module 11 uses JY-901 modules.JY-901 modules integrate high-precision gyroscope,
Accelerometer, geomagnetic field sensors, can under dynamic environment accurate output module current pose, attitude measurement accuracy 0.01
Degree, stability is high, and performance is even better than the inclinator of certain professions.JY-901 inside modules carry voltage stable circuit, work
Make voltage 3v~6v, pin level is compatible with the embedded system of 3.3V/5V.Support two kinds of digital interfaces of serial ports and IIC, IIC connects
Mouth supports full speed 400K rates.Retain 4 road ECP Extended Capabilities Ports, can be respectively configured as simulation input, numeral input, numeral output,
The functions such as PWM outputs, and have GPS concatenation abilities.
The sound acquisition module 6 uses ATK-VS1053MP3 modules.ATK-VS1053MP3 modules are a high-performance
Audio coding decoding module using VS1053B as master chip, is supported：The audios such as MP3/WMA/OGG/WAV/FLAC/MIDI/AAC
The decoding of form, and support：High low pitch section and EarSpeaker Spaces are supported in the recording of OGG/WAV audio formats
Setting, function are very powerful.Module is communicated by SPI interface with external microcontroller.
The voice synthetic module 7 uses XFS5152 chips.XFS5152CE chips are a highly integrated of HKUST News
The chipspeech of degree is, it can be achieved that Chinese, English phonetic synthesis；And voice coding, decoding function are integrated with, it can support user
It is recorded and is played.The speech identifying function of lightweight is integrated with, supports the identification of 30 order words, and supports user's
Order word customized demand.It supports the synthesis of arbitrary Chinese text, English text, and supports Chinese and English is mixed to read；Support voice coder
Decoding function, user directly can be recorded and be played using chip.Chip interior integrates 80 kinds of common prompt sound effects, is suitble to
Several scenes use.
The sound identification module 8 uses LD3320 chips.LD3320 integrated chips voice recognition processor and some
External circuit, including ADC, DAC, microphone interface, sound output interface etc..The chip does not need to external any companion chip
Such as Flash, RAM are directly integrated in existing product, you can to realize speech recognition/acoustic control/good in interactive function.
The ZigBee module 10 uses CC2530 chips.CC2530 chips are the ZigBee standard cores that TI companies release
Piece is applied suitable for 2.4GHz, IEEE802.15.4, ZigBee and RF4CE.CC2530 includes RF transceivers, and industrial standard increases
Epistasis 8051MCU, programmable flash memory, 8KB RAM and other functions, can be widely used in 2.4-GHzIEEE802.15.4
System, the distant control systems of RF4CE, ZigBee systems, family/building automation, lighting system, Industry Control and monitoring, it is low
Power consumption wireless sensor network, consumer electronics and health care.
The power module 12 uses LM2596 chips.LM2596 chips are the 3A electricity of National Semiconductor's production
Output buck switching mode integrated voltage-stabilized chip is flowed, it includes fixed oscillator (150KHZ) and benchmark voltage-stablizer (1.23v),
And with perfect protection circuit, current limit, Thermal shutdown circuit etc..Only need few peripheral components can structure using the device
Into efficient regulator circuit.What is provided has：Multiple voltage class products such as 3.3V, 5V, 12V and adjustable (- ADJ).
The clock module 13 uses DS1302 chips.DS1302 chips are that having for DALLAS companies of U.S. release is trickle
The low-power consumption real-time timepiece chip of electric current charging ability, can to year, month, day, Sunday, when, minute, second carry out timing, and with intercalation
The multiple functions such as year compensation.Data and clock information can be kept when less than 1 μ W, and with double tube-legs main power source and standby electricity
Source, the features such as may be programmed trikle charger and add the buffer of 7 bytes.
The STM32 one-chip computer modules respectively with sound acquisition module, voice synthetic module, sound identification module, satellite
Locating module, nine axis movement sensor modules, drive module, ultrasonic distance measuring module, ZigBee module are connected with clock module,
Survey area ambient sound is acquired by sound acquisition module, is exchanged by voice synthetic module with indicator of trapped personnel and obtains information,
Judge that survey area with the presence or absence of indicator of trapped personnel, drives aircraft flight by drive module, passes through by sound identification module
Nine axis movement sensors control aircraft flight direction, judges surrounding whether there are obstacles by ultrasonic distance measuring module, leads to
Cross satellite positioning module obtain current position coordinates, by ZigBee module realize information transmit, by clock module record by
The data acquisition time of oppressive member.In short, the STM32 one-chip computer modules receive and handle coupled sound collection mould
Block, voice synthetic module, sound identification module, satellite positioning module, nine axis movement sensor modules, drive module, ultrasonic wave
After range finder module, ZigBee module, clock module information, analysis and processing information, judge region whether there is indicator of trapped personnel.Work as presence
During indicator of trapped personnel, the information of indicator of trapped personnel is acquired, and acquisition information Wireless transceiver is gone back into appointed place.The power module difference
It is transported with STM32 one-chip computer modules, sound acquisition module, voice synthetic module, sound identification module, satellite positioning module, nine axis
Dynamic sensor assembly, drive module, ultrasonic distance measuring module, ZigBee module are connected with clock module, it is possible to provide 12V's and 5V
Supply voltage.
In the technical solution of the indicator of trapped personnel information collection aircraft of the utility model, used various components are existing
There is existing hardware device in technology, each function module therein is commercial product, by the utility model cleverly
Combination can obtain the technique effect of the utility model, therefore, in the technical solution of the utility model not include any for side
The improvement of method.
Employ the indicator of trapped personnel information collection aircraft in the utility model, the autonomous flight in major disaster region,
By voice recognition and synthetic technology, the calling for help language of indicator of trapped personnel is identified, with indicator of trapped personnel human-computer dialogue, collect indicator of trapped personnel
Information；After the covering for completing monitoring region perceives, communicated, sent certainly with data collection facility using sensor network technology
The indicator of trapped personnel data of body acquisition；This programme combining wireless senses network technology and sound treatment technology, can not using rescue personnel
The gold rescue cycle in time of arrival, the automatic information collection for carrying out indicator of trapped personnel and health estimation work, are later rescue personnel
Related data is provided into disaster-stricken scene, so as to make up the deficiency of current existing auxiliary rescue system, improves rescue to the maximum extent
Efficiency is helped, reduces the death rate of indicator of trapped personnel, avoids the generation of more domestic tragedies.
In this description, the utility model is described with reference to its specific embodiment.It but it is clear that still can be with
The spirit and scope that various modification can be adapted and converts without departing from the utility model.Therefore, the description and the appended drawings should be considered as
It is illustrative and not restrictive.
Claims (9)
1. a kind of indicator of trapped personnel information collection aircraft, which is characterized in that including aircraft skin, set on the aircraft skin
Hollow-cup motor module, motor drive module and ultrasonic distance measuring module are equipped with, the aircraft skin is internally provided with
STM32 one-chip computer modules, sound acquisition module, voice synthetic module, sound identification module, satellite positioning module, communication module,
Nine axis movement sensor modules, power module and clock module；
The motor drive module is connected with the hollow-cup motor module, and the power module is respectively the motor driving
Module, STM32 one-chip computer modules, sound acquisition module, voice synthetic module, sound identification module, is defended ultrasonic distance measuring module
Star locating module, communication module, nine axis movement sensor modules and clock module power supply, the STM32 one-chip computer modules difference
With the motor drive module, ultrasonic distance measuring module, sound acquisition module, voice synthetic module, sound identification module, satellite
Locating module, communication module, nine axis movement sensor modules are connected with clock module.
2. indicator of trapped personnel information collection aircraft according to claim 1, which is characterized in that the hollow-cup motor module
It it is four, the hollow-cup motor module is respectively arranged at four wings of aircraft；The ultrasonic distance measuring module is four, described
Ultrasonic distance measuring module is respectively arranged at the side of the aircraft skin.
3. indicator of trapped personnel information collection aircraft according to claim 1, which is characterized in that the STM32 microcontrollers mould
Block uses STM32F103C8 chips.
4. indicator of trapped personnel information collection aircraft according to claim 1, which is characterized in that the motor drive module is adopted
With 2SD315AI IGBT driving boards.
5. indicator of trapped personnel information collection aircraft according to claim 1, which is characterized in that nine axis movement sensor
Module uses JY-901 modules.
6. indicator of trapped personnel information collection aircraft according to claim 1, which is characterized in that the sound acquisition module is adopted
With ATK-VS1053MP3 modules.
7. indicator of trapped personnel information collection aircraft according to claim 1, which is characterized in that the voice synthetic module is adopted
With XFS5152 chips.
8. indicator of trapped personnel information collection aircraft according to claim 1, which is characterized in that the sound identification module is adopted
With LD3320 chips.
9. indicator of trapped personnel information collection aircraft according to claim 1, which is characterized in that the communication module is
ZigBee module, the ZigBee module use CC2530 chips.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721747808.1U CN207488769U (en) | 2017-12-14 | 2017-12-14 | Indicator of trapped personnel information collection aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721747808.1U CN207488769U (en) | 2017-12-14 | 2017-12-14 | Indicator of trapped personnel information collection aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207488769U true CN207488769U (en) | 2018-06-12 |
Family
ID=62458708
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201721747808.1U Expired - Fee Related CN207488769U (en) | 2017-12-14 | 2017-12-14 | Indicator of trapped personnel information collection aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207488769U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109753078A (en) * | 2019-01-31 | 2019-05-14 | 浙江大学 | Remote control method based on the unmanned vehicle that GPS positioning and spatial pose resolve |
| CN113933871A (en) * | 2021-10-15 | 2022-01-14 | 贵州师范学院 | Flood disaster detection system based on unmanned aerial vehicle and Beidou positioning |
-
2017
- 2017-12-14 CN CN201721747808.1U patent/CN207488769U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109753078A (en) * | 2019-01-31 | 2019-05-14 | 浙江大学 | Remote control method based on the unmanned vehicle that GPS positioning and spatial pose resolve |
| CN113933871A (en) * | 2021-10-15 | 2022-01-14 | 贵州师范学院 | Flood disaster detection system based on unmanned aerial vehicle and Beidou positioning |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20180612 Termination date: 20191214 |