CN104483987B - Unmanned plane is left a blank monitoring system - Google Patents
Unmanned plane is left a blank monitoring system Download PDFInfo
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- CN104483987B CN104483987B CN201410835651.2A CN201410835651A CN104483987B CN 104483987 B CN104483987 B CN 104483987B CN 201410835651 A CN201410835651 A CN 201410835651A CN 104483987 B CN104483987 B CN 104483987B
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Abstract
A kind of unmanned plane is left a blank monitoring system, at unmanned plane top equipped with emergent buffering parachute；Install semicircle propeller protector additional between upper and lower two propellers of each pair；On carry bar, carry two video cameras and four 100 watts of LED；It is also equipped with the high definition minisize pick-up head of two adjustable-angles in unmanned plane bottom；In the bottom of unmanned plane equipped with circular unmanned machine base；Launching platform frame positioned at ground is in dock shape with unmanned machine base；In the bottom of launching platform frame equipped with power supply and video line rolling frame, the power line inlet wire on power supply and video line rolling frame is terminated with direct current voltage regulator；It is additionally provided with induction machine and remote pilot box.The present invention has good illumination functions, and shooting picture is clear；Using ground power supply system and audio video synchronization download system, monitoring of can leaving a blank for a long time；Using induction machine device, motor automatic sensing unmanned plane can be allowed highly to come automatically to rotate, folding and unfolding electric wire is so that electric wire has obtained reasonable maximization use.
Description
Technical field
The invention belongs to monitoring field of taking photo by plane, the monitoring system more particularly, it relates to a kind of unmanned plane is left a blank.
Background technology
Advancing by leaps and bounds with national economic development, resource investigation and environmental monitoring work are more and more important, duty cycle
Shorter and shorter, conventional satellite and air remote sensing means are difficult to meet application demand.In recent years, low-altitude remote sensing dynamic monitoring and emergent
Monitor and be mainly used in the multiple emergency monitoring of dynamic monitoring and unexpected incidents etc. repeatedly of small range, and large scaled cartography
Demand, these detection requirement remote sensing obtain system to be possessed：1st, coverage count ability；2nd, wave band, resolution and when suitable
Spatial data capture ability；3rd, the offer ability of quantitative data；4th, high-precision fixed capability.Realizing of this target is non-single flat
Platform or sensor can be competent at.Due to being affected by factors such as satellite recursion period, spatial domain use and weathers, remotely-sensed data source
Ensure the bottleneck problem having become its application of restriction.
All kinds of natural disaster of modern society and accident take place frequently, if can not understand in time, the state of affairs is in progress, and can seriously limit
To the rescue assessment of disaster and the control process to accident, thus causing even more serious casualties and economic loss,
Therefore in the urgent need to a kind of scope is wide, the no high tracking system real-time dynamic of dead angle, mobility strong, synchronizing information.Unmanned plane
The development of technology, its application surface is more and more wider, all embodies indispensable importance in civil area and military domain, especially
Application in terms of aeroplane photography is more and more extensive, has become the master of current development as aeroplane photography platform using unmanned plane
Stream.But existing unmanned plane does not possess the function of illumination, the picture shooting out under conditions of night or light are bad compares
Fuzzy, very big trouble is brought to taking photo by plane；Even if in the unmanned plane carrying illumination apparatus at work, also due to on-board batteries
Capacity limit, leads to the working time extremely short it is impossible to play monitoring unmanned effect.
Content of the invention
Present invention aim to solution problem above, a kind of unmanned plane is provided to leave a blank monitoring system, it has very well
Illumination functions, shooting picture is clear；Monitoring system can steadily shoot for a long time, simultaneously can be by sensing the height of unmanned plane
Degree automatic deploying and retracting electric wire is so that unmanned plane disclosure satisfy that scope is wide, no high the moving in real time of dead angle, mobility strong, synchronizing information
State monitors.
The present invention provide technical scheme be：A kind of unmanned plane is left a blank monitoring system, and it includes unmanned plane, GPS location system
System, propeller, gyro sensor, video camera, the tilt-top of fixing camera；It is characterized in that：Each spiral shell of unmanned plane
Rotation oar is designed to upper and lower two propellers, respectively by upper and lower propeller Motor drive；At unmanned plane top equipped with emergent buffering
Parachute；Install outside semicircle propeller protector additional between upper and lower two propellers of each pair；Set up separately in unmanned plane lower half
There is carry bar, carry two video cameras and four 100 watts of LED on carry bar；It is externally provided with camera lens in camera lens
Wiper；It is also equipped with the high definition minisize pick-up head of two adjustable-angles in unmanned plane bottom, on high definition minisize pick-up head both sides
30 watts of spotlight LED lamps equipped with adjustable-angle；In the bottom of unmanned plane equipped with circular unmanned machine base；Rising positioned at ground
Winged paralell is in round table-like, and the upper plane of round platform is in concave groove type ring-type, and unmanned machine base circular with aircraft is in dock shape；?
It is integrated with portable electric power system on described launching platform frame；In the bottom of launching platform frame equipped with power supply and video line
The power supply being wound around in rolling frame, power supply and video line rolling frame and video line pass through the upper hole of launching platform frame and unmanned plane base holes to connect
Connect power input and the camera video outfan of unmanned plane；It is provided with transmission of video in the side of power supply and video line rolling frame to connect
Mouthful, the power line inlet wire on power supply and video line rolling frame is terminated with direct current voltage regulator, according to the high low-key of electric wire lift-off
The height of section supply voltage；It is additionally provided with induction machine and remote pilot box；Faradism arbor is contained in power supply and video line rolling frame
Rotating shaft at；Described induction machine highly to control the receipts of power supply and video line and to put by sensing unmanned plane；Described 100
Watt LED adjustable-angle, be additionally provided with the patten transformation program of lamp, be respectively scattering search pattern；Optically focused locking mode；Rescue
Help quick-fried sudden strain of a muscle pattern；Described remote pilot box is provided with a key and takes off and lifting key, decline key, a key return key.
The technical scheme being provided using the present invention, compared with prior art, has following remarkable result：
（1）The present invention, using illumination aircraft device, has good illumination functions, shooting picture is clear；
（2）The present invention adopts ground power supply system and audio video synchronization Transmission system, monitoring of can leaving a blank for a long time；
（3）The present invention adopts voltage self-checking device, automatically adjusts DC voltage according to aircraft altitude, overcomes electric wire
The resistance that length change leads to increases or reduces it is ensured that being aircraft and the offer stabilized power source supply of airborne electrical equipment.
（4）The present invention is using rain cover and camera lens wiper it is ensured that monitoring unmanned function also can work in the rainy day.
（5）The present invention adopts induction machine device, motor automatic sensing unmanned plane can be allowed highly to come automatically to rotate, folding and unfolding
Electric wire is so that electric wire has obtained reasonable maximization use.Unmanned plane is made to be capable of scope by apparatus above wide, no dead
The high real-time dynamic monitoring of angle, mobility strong, synchronizing information.
Brief description
Fig. 1 is the superstructure schematic diagram of the present invention.
Fig. 2 is substructure schematic diagram of the present invention.
In figure：1st, rain cover and emergent buffering parachute；2nd, upper and lower propeller motor；3rd, propeller protector；4th, carry
Bar；5th, power supply and video line；6th, unmanned machine base；7th, camera lens wiper；8th, 100 watts of LED；9th, high definition minisize pick-up head；10、
30 watts of spotlight LED lamps；11st, launching platform frame；12nd, video transmission interface；13rd, power supply and video line rolling frame；14th, DC voltage is adjusted
Section device；15th, remote pilot box；16th, a key takes off and lifting key；17th, decline key；18th, a key return key；19th, faradism arbor.
Specific embodiment
A kind of unmanned plane that can be seen that the present invention from Fig. 1 and Fig. 2 is left a blank monitoring system, and it includes rain cover, unmanned
Machine, GPS positioning system, propeller, gyro sensor, video camera, the tilt-top of fixing camera.Unmanned plane is using up and down
Double dynamical design, each propeller is designed to upper and lower two propellers, is driven by upper and lower propeller motor 2 respectively；One is to strengthen
Aircraft lifting capacity, two be to reduce frame further, improves the portability transporting transport；Three is to improve attitude of leaving a blank
Stability it is ensured that monitor video is smooth；Four have been an up aircraft safety, it is to avoid the aircraft that a certain electrical fault leads to is unbalance
Fall.At unmanned plane top equipped with emergent buffering parachute 1, when aircraft abnormal, automatic identification simultaneously ejects parachute,
The crowd on ground more protected by protection aircraft.Install outside semicircle propeller protector 3 additional between upper and lower two propellers of each pair,
One is to ensure that in transport, propeller is not subject to accidental damage, and two is awing to ensure that propeller does not touch foreign body, and three is to avoid no
Man-machine burst accidental falling leads to the oar of high-speed rotation to injure ground staff.It is provided with carry bar 4 in unmanned plane the latter half, hang
Carry carry on bar and two video cameras and four 100 watts of LED 8, carry bar acts the effect formed a connecting link, and for
Can be with conveniently fast disassembling；100 watts of LED adjustable-angles, searching and rescuing for ground provides visible light source, and unmanned plane is additionally provided with simultaneously
The patten transformation program of lamp, is scattering search pattern respectively；Optically focused locking mode；Rescue quick-fried sudden strain of a muscle pattern.Outside camera lens
It is provided with camera lens wiper 7, unmanned plane overhead rear lens have insecticide foreign body or have fog, raindrop, using camera lens windscreen wiper, can remove miscellaneous
Thing or rainwater.It is also equipped with the high definition minisize pick-up head 9 of two adjustable-angles in unmanned plane bottom, in high definition minisize pick-up head 9
Equipped with 30 watts of spotlight LED lamps 10 of adjustable-angle, high definition minisize pick-up head 9 and 30 watts of spotlight LED lamps 10 can same steps on both sides
Section angle, ensures photographic head shooting effect.In the bottom of unmanned plane equipped with circular unmanned machine base 6, for when landing just
Fall frame in the launching platform frame 11 positioned at ground；Launching platform frame 11 is in round table-like, and the upper plane of round platform is in concave groove type ring-type, with
The circular unmanned machine base 6 of aircraft is in docking shape, automatically locks, unmanned plane is difficult to tumble, ensure after being easy to unmanned plane landing
Unmanned plane and airborne electric equipment safety；In addition launching platform frame is integrated with electric power system further, carries more convenient.Taking off
The bottom of paralell 11 equipped with power supply and video line rolling frame 13, on power supply and video line rolling frame 13 be wound around power supply and video line 5
Connect power input and the camera video output of unmanned plane through the upper hole of launching platform frame 11 and unmanned machine base 6 hole
End.It is provided with video transmission interface 12 in the side of power supply and video line rolling frame 13, for exporting camera shooting and video signal.In power supply and
Power line inlet wire in video line rolling frame 13 is terminated with direct current voltage regulator 14, according to the height regulation power supply electricity of electric wire lift-off
The height of pressure.It is further provided with induction machine and remote pilot box 15；Faradism arbor 19 is contained in power supply and video line rolling frame 13
Rotating shaft at, induction machine highly to control the receipts of power supply and video line 5 and to put by sensing unmanned plane.Remote pilot box
15 are provided with a key takes off and lifting key 16, decline key 17, a key return key 18.
Claims (1)
1. a kind of unmanned plane is left a blank monitoring system, and it includes unmanned plane, GPS positioning system, propeller, gyro sensor, takes the photograph
Camera, the tilt-top of fixing camera；It is characterized in that：Each propeller of unmanned plane is designed to upper and lower two spirals
Oar, respectively by upper and lower propeller motor（2）Drive；At unmanned plane top equipped with emergent buffering parachute（1）；In each pair upper and lower two
Outside semicircle propeller protector is installed additional between propeller（3）；It is provided with carry bar in unmanned plane the latter half（4）, hang
Carry carry on bar and two video cameras and four 100 watts of LED（8）；It is externally provided with camera lens wiper in camera lens（7）；
It is also equipped with the high definition minisize pick-up head of two adjustable-angles in unmanned plane bottom（9）, high definition minisize pick-up head both sides equipped with
30 watts of spotlight LED lamps of adjustable-angle（10）；In the bottom of unmanned plane equipped with circular unmanned machine base（6）；Positioned at ground
Launching platform frame（11）In round table-like, the upper plane of round platform is in concave groove type ring-type, unmanned machine base circular with aircraft（6）
In docking shape；In described launching platform frame（11）On be integrated with portable electric power system；In launching platform frame（11）'s
Bottom is equipped with power supply and video line rolling frame（13）, the power supply of winding and video line on power supply and video line rolling frame（5）Pass through and take off
The power input of the upper hole of paralell and unmanned plane base holes connection unmanned plane and camera video outfan；In power supply and regard
The side of frequency line rolling frame is provided with video transmission interface（12）, the power line inlet wire on power supply and video line rolling frame is terminated with direct current
Voltage regulator（14）, the height of the height regulating power source voltage according to electric wire lift-off；It is additionally provided with induction machine and remote control control
Box processed（15）；Faradism arbor（19）It is contained at power supply and the rotating shaft of video line rolling frame；Described induction machine passes through sensing no
The man-machine receipts highly to control power supply and video line with put；The LED of described 100 watts（8）Adjustable-angle, is additionally provided with lamp
Patten transformation program, is scattering search pattern respectively；Optically focused locking mode；Rescue quick-fried sudden strain of a muscle pattern；Described remote pilot box
（15）It is provided with a key to take off and lifting key（16）, decline key（17）, a key return key（18）.
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| CN201410835651.2A CN104483987B (en) | 2014-12-29 | 2014-12-29 | Unmanned plane is left a blank monitoring system |
Applications Claiming Priority (1)
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| CN201410835651.2A CN104483987B (en) | 2014-12-29 | 2014-12-29 | Unmanned plane is left a blank monitoring system |
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| CN104483987A CN104483987A (en) | 2015-04-01 |
| CN104483987B true CN104483987B (en) | 2017-03-01 |
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| CN104986340B (en) * | 2015-06-15 | 2017-04-05 | 西华大学 | A kind of multi-rotor aerocraft emergency protection system and method |
| KR101708037B1 (en) * | 2015-11-16 | 2017-02-27 | 주식회사 앤다스 | Drone connected cctv apparatus and method for photographing image thereby |
| GB2556644B (en) | 2017-02-28 | 2018-11-28 | Matthew Russell Iain | Unmanned aerial vehicles |
| CN106970639A (en) * | 2017-03-15 | 2017-07-21 | 武汉理工大学 | A kind of harbour outdoor scene monitoring system and method based on unmanned aerial vehicle platform |
| CN106681360B (en) * | 2017-03-21 | 2023-05-02 | 合肥佳讯科技有限公司 | Multi-rotor unmanned aerial vehicle with high-brightness aerial illumination |
| CN107765704A (en) * | 2017-09-18 | 2018-03-06 | 广东泰高新技术发展有限公司 | The unmanned machine automatic drive system of fixed-wing |
| CN107757844B (en) * | 2017-10-21 | 2019-05-28 | 天津黎明时代信息技术有限公司 | It is a kind of marine to track down and arrest and relief unmanned plane |
| CN108583917A (en) * | 2018-05-11 | 2018-09-28 | 深圳市玖品空气净化科技有限公司 | A kind of recognition of face flight equipment for park monitoring |
| CN111147727A (en) * | 2020-01-16 | 2020-05-12 | 冀湘元 | Three-dimensional space mobile monitoring system and installation, use and accurate landing method |
| CN111503440B (en) * | 2020-03-17 | 2021-07-09 | 熊新明 | Forest fire prevention monitoring and patrolling system |
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| US8774982B2 (en) * | 2010-08-26 | 2014-07-08 | Leptron Industrial Robotic Helicopters, Inc. | Helicopter with multi-rotors and wireless capability |
| CN102730189B (en) * | 2011-03-29 | 2018-02-23 | 郑鹏 | It is peculiar to vessel to fly to hang lifesaving appliance and its control method |
| CN202170018U (en) * | 2011-07-15 | 2012-03-21 | 东华大学 | Small-sized perpendicular taking off and landing unmanned plane for monitoring and fire fighting |
| US8907846B2 (en) * | 2013-02-05 | 2014-12-09 | King Fahd University Of Petroleum And Minerals | Single-antenna direction finding system for multi-rotor platforms |
| CN203864994U (en) * | 2014-05-12 | 2014-10-08 | 国家电网公司 | Unmanned patrolling airplane for power transmission line |
| CN204013920U (en) * | 2014-08-29 | 2014-12-10 | 马鞍山市靓马航空科技有限公司 | A kind of night search and rescue, search system |
| CN104210659B (en) * | 2014-09-15 | 2016-01-06 | 金陵科技学院 | A kind of skyscraper cleaning unmanned plane |
| CN204331478U (en) * | 2014-12-29 | 2015-05-13 | 马鞍山市赛迪智能科技有限公司 | Unmanned plane is left a blank supervisory system |
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Effective date of registration: 20191227 Address after: 211100 science and technology innovation center, No.18, Tiancheng Road, Binjiang Economic Development Zone, Jiangning District, Nanjing City, Jiangsu Province Patentee after: Nanjing Liangma Geographic Information Technology Co., Ltd Address before: 243000 North Road in Anhui high tech Zone Chihu Huo sparkle city in Ma'anshan province 1699 Patentee before: MA'ANSHAN SAIDI INTELLIGENT TECHNOLOGY CO., LTD. |