CN206318028U - A kind of Information Acquisition System based near space floating platform - Google Patents
A kind of Information Acquisition System based near space floating platform Download PDFInfo
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- CN206318028U CN206318028U CN201621093929.4U CN201621093929U CN206318028U CN 206318028 U CN206318028 U CN 206318028U CN 201621093929 U CN201621093929 U CN 201621093929U CN 206318028 U CN206318028 U CN 206318028U
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- floating platform
- near space
- space floating
- mav
- information acquisition
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Abstract
The utility model provides a kind of Information Acquisition System based near space floating platform, including near space floating platform, delivery device, multiple MAVs and satellite, and near space floating platform is used to carry delivery device to specified location；Delivery device is used to carry multiple MAVs, and delivery device is additionally operable to deliver multiple MAVs after reaching specified location；Multiple MAVs are used to land respectively to the peripheral location of ground target, carry out information gathering, and the information of collection is sent to satellite.The near space floating platform that the utility model is used has stronger load-carrying ability, and accurate, snugly can deliver around unmanned plane to objective, and micro-unmanned function reliably carries out information gathering and transmission.
Description
Technical field
The utility model belongs to unmanned plane field, more particularly to a kind of acquisition of information system based near space floating platform
System.
Background technology
The emphasis of 21 century war is information war.The core of information war is the acquisition power around information, control and made
With power.On Information Battlefield, information turns into key element that is leading and dominating battlefield, and warfare decision leans on information, commander's control
Dependency Specification, precision strike needs information.The purpose of this utility model is to develop a kind of available and safe and reliable information conscientiously
Acquisition methods.
Unmanned plane (Unmanned Aerial Vehicle, UAV) is one of main channel of wartime acquisition of information, is passed through
Prolonged monitoring flight, ground image data can be obtained exactly for my army's decision-making, is a kind of reason in enemy control zone
The strategic arms platform thought.The characteristics of when unmanned plane for performing this kind of acquisition of information task at present often navigates with superaltitude, length,
These features are also the bottleneck problem in unmanned plane research and development, and it is difficult the crux for obtaining perfect solution in a short time to be, and this
Plant unmanned plane cost often very high, once it will be undoubtedly great loss to be shot down by enemy.
Another prior art uses abandonable after-use hidden autonomous flight SUAV (Close-in
Covert Autonomous Disposable Aircraft, CICADA), as shown in figure 1, two frame CICADA are divided when using
Other carry in Tempest unmanned plane wings bottom, using meteorological balloon (Weather Balloon, WB) carry Tempest nobody
Machine goes up to the air, and reaches and Tempest unmanned planes are discharged after certain altitude, and after one segment distance of flight, CICADA departs from Tempest unmanned planes
Gliding flies into enemy army rear, obtains information by the sensor carried on machine and is forwarded the information to by Tempest unmanned planes
Satellite.Such scheme has as a drawback that：
(1) by the use of meteorological balloon as female platform, its load-carrying ability is limited, seriously constrains the extension of acquisition of information class load
Carry quantity；
(2) meteorological balloon can only be floated with the wind after granting, it is impossible to kept height, therefore can not be flown to mesh using natural wind
Punctuate；
(3) dispensing that enemy-occupied area carries out acquisition of information unmanned plane is flown into using Tempest unmanned planes, it is disguised poor, easily
Detected and then shot down by enemy radar；
(4) the unmanned plane quantity for being used for execution information acquisition task is very few, in the case of by enemy's discovery or component failure
It is easily caused mission failure；
(5) information transfer chain relies on Tempest unmanned planes, and unmanned plane, which is shot down or failed, will all cause mission failure.
Utility model content
(1) technical problem to be solved
In view of the above problems, the purpose of this utility model is to provide a kind of information based near space floating platform to obtain
System is taken, with stronger load-carrying ability, accurate, snugly can be delivered around unmanned plane to objective, and can reliably enter
Row information is gathered and transmitted.
(2) technical scheme
The utility model provides a kind of Information Acquisition System based near space floating platform, and system includes near space
Floating platform, delivery device, multiple MAVs and satellite, multiple MAVs are connected with satellite communication, multiple miniature
Unmanned plane is located in delivery device, and delivery device is connected near space floating Platform Machinery, wherein,
Near space floating platform is used to carry delivery device to specified location；
Delivery device is used to carry multiple MAVs, delivery device be additionally operable to reach delivered after specified location it is multiple micro-
Type unmanned plane；
Multiple MAVs are used to land respectively to the peripheral location of ground target, carry out information gathering, and will adopt
The information of collection is sent to satellite.
Further, specified location includes the horizontal level apart from the horizontal range of ground target one, and apart from ground target one
The upright position of vertical range；Delivery device using upright position be height, using ground target as the center of circle, using horizontal level for partly
Multiple MAVs are delivered by footpath respectively, the position to around ground target so that multiple MAVs land respectively
Put.
Further, upright position is more than 20km apart from the vertical range of ground target.
Further, delivery device hangs near space floating platform lower by flexible cablet.
Further, flight control system, sensor and communication equipment are provided with MAV, wherein：
Flight control system is used for after the MAV is launched, and control MAV flies to ground target
Peripheral location；
Sensor is used to carry out information gathering；
Communication equipment is used for and satellite communication, and the information of collection is sent to satellite.
Further, the body of MAV is a printed circuit board (PCB), flight control system, sensor and communication equipment collection
Into on a printed circuit.
Further, MAV also includes an energy battery, for being powered to printed circuit board (PCB), on energy battery
It is pasted with insulation resistor disc.
Further, MAV also includes a self-desttruction equipment, for after energy battery exhausts, entering to printed circuit board (PCB)
Row is destroyed.
Further, sensor is the one or more in sound transducer, shock sensor and magnetometric sensor.
Further, near space floating platform is one kind in aerostat, super-pressure balloon, stratospheric airship.
(3) beneficial effect
The Information Acquisition System based near space floating platform that the utility model is provided, with advantages below：
(1) the utility model uses near space floating platform as female platform, and its load-carrying ability is obviously improved, and can be taken
With more MAVs, the probability of success of task is improved；
(2) the near space floating platform used in the utility model has autonomous control ability, can stablize a certain
On height, wind action target point is utilized；
(3) MAV, the floating of highly concealed type are directly delivered using near space floating platform in the utility model
The disguise and security that combine the system of improving of platform and MAV；
(4) sow formula impression information into batch using near space floating platform in the utility model and obtain unmanned plane, nothing
Man-machine quantity is more, distributed areas wide, and enemy is difficult to pull out all unmanned planes, improves the probability of success of task；
(5) MAV and satellite direct communication in the utility model, simplify information transfer link, improve information
The safety and reliability of transmission.
Brief description of the drawings
Fig. 1 is the schematic diagram of acquisition of information in the prior art.
Fig. 2 is the structural representation for the Information Acquisition System that the utility model is provided.
Fig. 3 is the structural representation for the MAV that the utility model is provided.
Fig. 4 is the fundamental diagram for the Information Acquisition System that the utility model is provided.
Embodiment
For the purpose of this utility model, technical scheme and advantage is more clearly understood, below in conjunction with specific embodiment, and
Referring to the drawings, the utility model is further described.
Fig. 2 is the structural representation for the Information Acquisition System that the utility model is provided, as shown in Fig. 2 Information Acquisition System
Formula delivery device 2, flexible cablet 3, multiple MAVs 4 and satellite (figure are sowed including near space floating platform 1, high-altitude
Do not show), specifically, near space floating platform 1 is near space aerostat, formula is sowed in high-altitude by it by flexible cablet 3
Delivery device 2 is hung.Near space aerostat is filled with helium when working, and high-altitude can be sowed to formula delivery device 2 and risen to
More than 20km near spaces region, then sows the safety of formula delivery device 2 by high-altitude using natural wind and delivers to high-altitude placement position,
Wherein, multiple MAVs 4 are placed in high-altitude and sowed in formula delivery device 2, for example, can be positioned over 100 frame MAVs 4
High-altitude is sowed in formula delivery device 2, to be delivered in specified location.It is taking for MAV that formula delivery device is sowed in high-altitude
Carrying platform, when reaching the specified location delivered, bottom hatch door is opened, and multiple MAVs can be sowed to formula throwing in batches
Put.
Fig. 3 is the structural representation for the MAV that the utility model is provided, as shown in figure 3, the wing of MAV 4
Face is shaped as graceful (Inverse Zimmerman) flat profile of anti-Zimmer that aspect ratio is 1.2, and body 41 is that thickness is 1.5mm
Printed circuit board (PCB) (PCB).MAV includes flight control system 42, the sensor 43 being integrated on printed circuit board (PCB) 41
And communication equipment 44.Wherein, energy battery is additionally provided with printed circuit board (PCB), for being powered to printed circuit board (PCB), so that print
It is pasted with flight control system 42, sensor 43 and the energy normal work of communication equipment 44 on printed circuit board 41, energy battery
Resistor disc is incubated, enables the normal work under high-altitude low temperature environment of MAV 4.In addition, MAV 4 also includes one
Individual self-desttruction equipment, for after energy battery exhausts, being destroyed to printed circuit board (PCB) 41, it is to avoid technology is revealed.
The electronic component that flight control system 42 is used is directly welded on pcb board, alleviates additional structure
Weight.Further, since MAV does not carry power source, after MAV 4 is launched, flight control system 42 is controlled
The flaperon gliding flight of MAV 4.
Sensor 43 is that a class size is small, lightweight information gathering instrument, is mounted on MAV and is used for performing
Acquisition of information task, the species of sensor 43 is more, such as sound transducer, shock sensor, magnetometric sensor etc., this practicality
It is new according to different task different sensors to be selected to be installed.
Communication equipment 44 is used for and satellite communication, and the information that sensor 43 is collected is sent to satellite, then by satellite
The reception center for being forwarded to ground carries out the subsequent treatments such as information analysis.
Fig. 4 is the fundamental diagram for the Information Acquisition System that the utility model is provided, as shown in figure 4, utilizing acquisition of information
What system execution information was obtained comprises the following steps that：
S1, the sensor 43 of respective type is selected according to task objective, and is integrated on MAV 4, is adjusted
The position of centre of gravity of MAV 4, makes it have compared with high lift-drag ratio；
S2, the energy battery position paste heat-preserving resistor disc on the printed circuit board (PCB) 41 of MAV 4, makes miniature nothing
Man-machine 4 can be in normal work under high-altitude low temperature environment；
S3,100 framves is adjusted the MAV 4 finished and sowed installed in high-altitude inside formula delivery device 2, pass through flexibility
High-altitude is sowed the stabilization of formula delivery device 2 and is suspended on the lower section of near space aerostat 1 by cablet 3；
S4, is filled with helium inside near space aerostat 1, and is discharged by ground infrastructure, makes to close on
Space aerostat 1 carries delivery device 2 and gone up to the air；
S5, according to the different principle of different height wind direction, by the weight for adjusting ballast near space aerostat 1
Amount, makes near space aerostat 1 stablize in favourable wind direction highly, horizontal target place；
S6,10 kilometers of distance objective place position in the horizontal direction, high-altitude is sowed the bottom hatch door of formula delivery device 2 and opened,
100 frame MAVs 4 are sowed into formula in batches to deliver；
S7, under flight control system 42 is guided on MAV 4,100 frame MAVs are public with objective 10
In be radius, respectively in different directions, different landing point slipped into around objective；
S8, after MAV 4 lands, turn on sensor 43 and execution information acquisition task；
S9, is collected into after effective information, is sent information to and defended by the communication equipment 44 carried on MAV 4
Star, and then passed the information on by satellite and be back to terrestrial information center；
S10, on MAV 4 after power depletion, starts self-desttruction equipment, printed circuit board (PCB) 41 is destroyed, kept away
Immune technology is revealed.
In summary, the Information Acquisition System based near space floating platform that the utility model is provided, due to using
Near space floating platform is as female platform, so that there is preferable load-carrying ability, meanwhile, near space floating platform has certainly
Main control ability, can stablize on a certain height, utilize wind action target point；Using the floating platform of highly concealed type
With the disguise and security that combine the system of improving of MAV；Using near space floating platform formula is sowed into batch
The MAV that supply volume is more, distributed areas are wide, improves the probability of success of task；MAV directly leads to satellite
Letter, simplifies information transfer link, improves the safety and reliability of information transfer.
Particular embodiments described above, has carried out entering one to the purpose of this utility model, technical scheme and beneficial effect
Step is described in detail, be should be understood that and be the foregoing is only specific embodiment of the utility model, is not limited to this
Utility model, all within spirit of the present utility model and principle, any modifications, equivalent substitutions and improvements done etc. all should be wrapped
It is contained within protection domain of the present utility model.
Claims (10)
1. a kind of Information Acquisition System based near space floating platform, it is characterised in that system includes near space floating
Platform, delivery device, multiple MAVs and satellite, the multiple MAV is connected with the satellite communication, described
Multiple MAVs are located in delivery device, and the delivery device is connected with the near space floating Platform Machinery, wherein,
The near space floating platform is used to carry the delivery device to specified location；
The delivery device is used to carry the multiple MAV, and the delivery device is additionally operable to reach after specified location and thrown
Put the multiple MAV；
The multiple MAV is used to land respectively to the peripheral location of ground target, carries out information gathering, and will adopt
The information of collection is sent to the satellite.
2. the Information Acquisition System according to claim 1 based near space floating platform, it is characterised in that the finger
Positioning is put including the horizontal level apart from the horizontal range of ground target one, and apart from the vertical position of the vertical range of ground target one
Put；The delivery device using the upright position be height, using the ground target as the center of circle, using the horizontal level for partly
Footpath, is delivered respectively to the multiple MAV, so that the multiple MAV lands to ground target respectively
Peripheral location.
3. the Information Acquisition System according to claim 2 based near space floating platform, it is characterised in that described to hang down
The vertical range of straight positional distance ground target is more than 20km.
4. the Information Acquisition System according to claim 1 based near space floating platform, it is characterised in that the throwing
Put device and near space floating platform lower is hung on by flexible cablet.
5. the Information Acquisition System according to claim 1 based near space floating platform, it is characterised in that described micro-
Flight control system, sensor and communication equipment are provided with type unmanned plane, wherein：
The flight control system is used for after the MAV is launched, and controls the MAV to fly to ground
The peripheral location of target；
The sensor is used to carry out information gathering；
The communication equipment is used for and satellite communication, and the information of collection is sent to the satellite.
6. the Information Acquisition System according to claim 5 based near space floating platform, it is characterised in that described micro-
The body of type unmanned plane is a printed circuit board (PCB), and the flight control system, sensor and communication equipment are integrated in the printing
On circuit board.
7. the Information Acquisition System according to claim 6 based near space floating platform, it is characterised in that described micro-
Type unmanned plane also includes an energy battery, and for being powered to the printed circuit board (PCB), guarantor is pasted with the energy battery
Warm resistor disc.
8. the Information Acquisition System according to claim 7 based near space floating platform, it is characterised in that described micro-
Type unmanned plane also includes a self-desttruction equipment, for after the energy battery exhausts, being destroyed to the printed circuit board (PCB).
9. the Information Acquisition System according to claim 5 based near space floating platform, it is characterised in that the biography
Sensor is the one or more in sound transducer, shock sensor and magnetometric sensor.
10. the Information Acquisition System according to claim 1 based near space floating platform, the near space floating
Platform is one kind in aerostat, super-pressure balloon, stratospheric airship.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621093929.4U CN206318028U (en) | 2016-09-29 | 2016-09-29 | A kind of Information Acquisition System based near space floating platform |
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| CN201621093929.4U CN206318028U (en) | 2016-09-29 | 2016-09-29 | A kind of Information Acquisition System based near space floating platform |
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| CN206318028U true CN206318028U (en) | 2017-07-11 |
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Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106347694A (en) * | 2016-09-29 | 2017-01-25 | 中国科学院光电研究院 | Information acquisition system based on near space floating platform |
| CN109141429A (en) * | 2018-09-03 | 2019-01-04 | 中国科学院工程热物理研究所 | The balloon borne solar energy unmanned plane launch process track design method of near space |
| CN111780797A (en) * | 2020-05-28 | 2020-10-16 | 中国人民解放军军事科学院国防科技创新研究院 | Simulation test device and method for space-air cooperative remote sensing system |
-
2016
- 2016-09-29 CN CN201621093929.4U patent/CN206318028U/en active Active
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106347694A (en) * | 2016-09-29 | 2017-01-25 | 中国科学院光电研究院 | Information acquisition system based on near space floating platform |
| CN106347694B (en) * | 2016-09-29 | 2018-08-10 | 中国科学院光电研究院 | A kind of Information Acquisition System based near space floating platform |
| CN109141429A (en) * | 2018-09-03 | 2019-01-04 | 中国科学院工程热物理研究所 | The balloon borne solar energy unmanned plane launch process track design method of near space |
| CN111780797A (en) * | 2020-05-28 | 2020-10-16 | 中国人民解放军军事科学院国防科技创新研究院 | Simulation test device and method for space-air cooperative remote sensing system |
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