CN103950536A - Unmanned helicopter system applicable to reconnaissance - Google Patents
Unmanned helicopter system applicable to reconnaissance Download PDFInfo
- Publication number
- CN103950536A CN103950536A CN201410182990.5A CN201410182990A CN103950536A CN 103950536 A CN103950536 A CN 103950536A CN 201410182990 A CN201410182990 A CN 201410182990A CN 103950536 A CN103950536 A CN 103950536A
- Authority
- CN
- China
- Prior art keywords
- module
- probe
- infrared
- unmanned helicopter
- infra
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
Links
Landscapes
- Optical Radar Systems And Details Thereof (AREA)
Abstract
The invention discloses an unmanned helicopter system applicable to reconnaissance and belongs to the field of tactical reconnaissance technologies. The unmanned helicopter system applicable to reconnaissance comprises a controller (1), a first paddle group control module (2), a second paddle group control module (3), a laser detecting module (4), an infrared sensing module (5), a probe rotation control module (6), a probe pitching control module (7), a wireless communication module (8), a GPS (Global Position System) positioning module (9), a video collecting module (10) and a gyroscope positioning module (11). Compared with the prior art, the unmanned helicopter system for reconnaissance has the characteristics of simple structure, reliable performance, convenience in operation and the like. By virtue of the unmanned helicopter, effective reconnaissance in various complex battlefield environments can be realized; the unmanned helicopter is capable of effectively monitoring and scouting dead zones which are incapable of being recognized by naked eyes and sending an alarm.
Description
Technical field
The invention belongs to tactical reconnaissance technical field, in particular, belong to a kind of unmanned aerial vehicle control system that utilizes infrared technology and laser technology to scout.
Background technology
The on-the-spot Intelligence Technology of battle reconnaissance and emergency situation is that combat troop, police force all need the practical problems of facing, and how effectively battlefield and emergency situation scene effectively to be scouted, to be a great problem of restriction field army and special policeman Force Reconnaissance.The battle reconnaissance system of field army should be the sky world trinity, i.e. reconnaissance satellite, scout (comprising scounting aeroplane, reconnaissance helicopter etc.), ground armored scout car and in particular cases by a small amount of scout, form moral investigation group.In prior art, always custom is paid attention to powerful a series of high-tech means such as space reconnaissance, has but ignored the vital function of traditional ground reconnaissance, and how some concealed targets being carried out effectively scouting inhibition is a great problem of the art.
Simultaneously along with social development, all kinds of disaster assistances that fire brigade faces are increasingly sophisticated, particularly some special rescues, conventional fire-fighting systems such as high-altitude, lofty mountains rescue, flood-fighting is difficult to meet rescue needs, all needs fire fighter emitting life danger to go deep into a line during rescue.For example, while having personnel to be confined in steep cliff somewhere, somewhere, high-altitude or flood-fighting, be confined in flood, or be difficult for being examined not by naked eyes by rescue group, during rescue, be all fire fighter emitting life danger carry rescue rope go to alone rescue, when stranded overlong time rescue difficulty is larger sometimes, also need not timing to carry water or food etc., how reducing firefighters rescue difficulty, reducing hazard to person, improve rescue efficiency is also a great problem.
Summary of the invention
The present invention, in order effectively to solve above technical matters, has provided a kind of scouting robot.
A kind of scouting unmanned helicopter system of the present invention, it is characterized in that, comprise controller, the first blade group control module, the second blade group control module, laser detection module, infra-ray sensing module, probe revolution control module, probe pitch control subsystem module, wireless communication module;
Described controller is electrical connected with described the first blade group control module, described the second blade group control module, described laser detection module, described infra-ray sensing detection module, described probe revolution control module, described probe pitch control subsystem module, described wireless communication module respectively;
Described infra-ray sensing module is electrical connected with the first infrared probe, the second infrared probe respectively, and described the first infrared probe and described the second infrared probe are arranged on flight body symmetrically; The infra-red detection amplitude angle A of described the first infrared probe is identical with the infra-red detection amplitude angle B of described the second infrared probe; The infra-red detection region S of described the first infrared probe
3infra-red detection region S with described the second infrared probe
4mutually intersect to form an infrared ray blind area region S
1an and infrared ray overlap-add region S
2, described infrared ray overlap-add region S
2angle C, described infrared ray blind area region S
1with described infrared ray overlap-add region S
2coaxially;
Described laser detection module comprises described Laser emission part and described laser pick-off part, receive direction and the described infrared ray overlap-add region S of the downrange of described Laser emission part, described laser pick-off part
2axis direction in the same way.
According to above-described scouting unmanned helicopter system, preferably, also comprise GPS locating module, described GPS locating module and described controller are electrical connected.
According to above-described scouting unmanned helicopter system, preferably, also comprise video acquisition module, described video acquisition module and described controller are electrical connected.
According to above-described scouting unmanned helicopter system, preferably, also comprise gyro locating module, described gyro locating module and described controller are electrical connected.
According to above-described scouting unmanned helicopter system, preferably, the receive direction of the admission direction of described video acquisition module and the downrange of described Laser emission part, described laser pick-off part is consistent.
According to above-described scouting unmanned helicopter system, preferably, described infrared ray overlap-add region S
2angle C be 4-50 degree.
Scouting of the present invention is surveillance drone helicopter by the control object of unmanned helicopter system, reconnaissance helicopter comprises the body that flies, the first blade group motor, the second blade group motor, scouting probe mechanism, probe turning motor, probe pitching motor, electrokinetic cell and control system recited above, and control system is controlled the first blade group motor, the second blade group motor, scouting probe mechanism, the turning motor of popping one's head in, the probe pitching motor that are arranged on flight body; The first blade group control module is connected to realize the control to the first blade group motor with the first blade group motor, the second blade group control module is connected to realize the control to the second blade group motor with the second blade group motor, the first blade group motor and the second blade group motor have completed the sporting flying of helicopter jointly.Probe revolution control module is connected to realize the control to probe turning motor with probe turning motor, and probe pitch control subsystem module is connected to realize the control to probe pitching motor with probe pitching motor; Adjusting probe turning motor and probe pitching motor is to adjust scouting probe mechanism in order to realize, and then makes probe obtain different collection orientation angles.Electrokinetic cell provides electric energy power for the first blade group motor, the second blade group motor, probe turning motor, probe pitching motor, and provides electric energy by voltage reduction module for the each several part in control system.Controller of the present invention is connected with wireless communication module, GPS locating module, video acquisition module, gyro locating module respectively, wireless communication module sends to controller by extraneous wireless remote control signals, the signal of the signal of GPS locating module, the signal of video acquisition module, gyro locating module can send to wireless communication module by controller, by wireless communication module, sends to extraneous wireless remote control control terminal.
That the present invention compared with prior art has is simple in structure, dependable performance, the feature such as easy to operate, easy to operate, by of the present invention nobody go straight up to scout and can realize the effective scouting to various Complex Battlefield Environments, can carry out effectively monitoring to the blind area of naked eyes None-identified and scout and send warning.
Accompanying drawing explanation
Accompanying drawing 1 is that the present invention scouts the schematic diagram one with unmanned helicopter system;
Accompanying drawing 2 is that the present invention scouts the schematic diagram two with unmanned helicopter system;
Accompanying drawing 3 is that the present invention scouts the schematic diagram three with unmanned helicopter system;
Accompanying drawing 4 is that the present invention scouts the schematic diagram four with unmanned helicopter system;
Accompanying drawing 5 is that the present invention scouts the schematic diagram with unmanned helicopter system;
Accompanying drawing 6 is structural representations of infra-ray sensing module of the present invention.
The specific embodiment
Fig. 1 is that the present invention scouts the schematic diagram one with unmanned helicopter system; Fig. 2 is that the present invention scouts the schematic diagram two with unmanned helicopter system; Fig. 3 is that the present invention scouts the schematic diagram three with unmanned helicopter system; Fig. 4 is that the present invention scouts the schematic diagram four with unmanned helicopter system.Scouting unmanned helicopter system of the present invention, nobody goes straight up to flight body on scout, the first blade group motor, the second blade group motor, scout probe mechanism, probe turning motor, probe pitching motor, electrokinetic cell and control system; Scouting probe mechanism is arranged on flight body, the motion of the first blade group motor and the second blade group motor co-controlling flight body, the first blade group motor provides power for Helicopter Main rotor provides the balance rotor that power, the second blade group motor are helicopter afterbody, probe turning motor and probe pitching motor control to be scouted the motion of probe mechanism and are scouted visual angle to adjust, and electrokinetic cell provides power for the first blade group motor, the second blade group motor, probe turning motor and probe pitching motor.The first blade group motor, the second blade group motor, probe turning motor, probe pitching motor, electrokinetic cell are all placed in interior of aircraft, do not show the first blade group motor, the second blade group motor, probe turning motor, probe pitching motor, electrokinetic cell in Fig. 1, Fig. 2, Fig. 3, Fig. 4.
Going straight up to scout flight body has motion characteristics flexibly and can guarantee infrared detection part and laser detection co-ordination partly; The body that flies in this preferred embodiment adopts double dynamical version, 1 pair of the first blade group control module 2 of controller and the second blade group control module 3 are coordinated control, and body moving, scouting to coordinate infrared detection part and laser detection part to carry out effectively monitoring to quilt scouting object along any direction and height can make to fly.Extraneous wireless remote control control terminal can carry out remote control to depopulated helicopter, and 1 pair of the first blade group control module 2 of middle controller of the present invention is identical with helicopter model control principle of the prior art with the principle that the second blade group control module 3 is coordinated control.
Fig. 5 be the present invention nobody go straight up to the structural representation of scout control system; Control system comprises controller 1, the first blade group control module 2, the second blade group control module 3, laser detection module 4, infra-ray sensing module 5, probe revolution control module 6, probe pitch control subsystem module 7, wireless communication module 8, GPS locating module 9, video acquisition module 10.
Controller 1 respectively with the first blade group control module 2, the second blade group control module 3, laser detection module 4, infra-ray sensing detection module 5, probe revolution control module 6, probe pitch control subsystem module 7, wireless communication module 8, GPS locating module 9, video acquisition module 10 is electrical connected, controller 1 is respectively to the first blade group control module 2, the second blade group control module 3, laser detection module 4, infra-ray sensing detection module 5, probe revolution control module 6, probe pitch control subsystem module 7, wireless communication module 8, GPS locating module 9, video acquisition module 10 is controlled, electrokinetic cell by voltage reduction module be respectively controller 1, the first blade group control module 2, the second blade group control module 3, laser detection module 4, infra-ray sensing detection module 5, probe revolution control module 6, probe pitch control subsystem module 7, wireless communication module 8, GPS locating module 9, video acquisition module 10 provides power supply, electrokinetic cell is placed in helicopter body.
The second blade group control module 3 and the first blade group motor are electrical connected to realize the control to the first blade group motor, the first blade group control module 2 and the second blade group motor are electrical connected to realize the control to the second blade group motor, by the control of the first blade group motor and the second blade group motor having been realized to flight body.Probe revolution control module 6 is connected to realize the control to probe turning motor with probe turning motor, probe pitch control subsystem module 7 is connected to realize the control to probe pitching motor with probe pitching motor, by having realized scouting the control of probe mechanism to the control of probe turning motor with to the control of probe pitching motor.
Infra-ray sensing module 5 is electrical connected with the first infrared probe 501, the second infrared probe 502 respectively, and the first infrared probe 501 and the second infrared probe 502 are arranged on the investigation probe below flight body symmetrically; The infra-red detection amplitude angle A of the first infrared probe 501 is identical with the infra-red detection amplitude angle B of the second infrared probe 502; The infra-red detection region S of the first infrared probe 501
3infra-red detection region S with the second infrared probe 502
4mutually intersect to form an infrared ray blind area region S
1an and infrared ray overlap-add region S
2, infrared ray overlap-add region S
2angle C, infrared ray blind area region S
1with infrared ray overlap-add region S
2coaxially.
Laser detection module 4 is electrical connected with Laser emission part 401, laser pick-off part 402 respectively, and Laser emission part 401 and laser pick-off part 402 are arranged near the mid point between the first infrared probe 501 and the second infrared probe 502; Laser emission part 401 and laser pick-off part 402 have obtained widespread use in the prior art, and Laser emission part 401 and laser pick-off part 402 directly adopt prior art.The receive direction of the downrange of the axis of the axis of the first infrared probe 501, the second infrared probe 502 and Laser emission part 401, laser pick-off part 402 is all positioned at same plane, can guarantee that like this common combination testing result of infrared ray and laser is optimum.Laser emission part 401, laser pick-off part 402, the axis of the first infrared probe 501, shown in the second infrared probe 502 concrete placement Fig. 4 on investigation probe, probe revolution control module 6 is connected to realize the control to probe turning motor with probe turning motor, probe pitch control subsystem module 7 is connected to realize the control to probe pitching motor with probe pitching motor, by having realized scouting the control of probe mechanism to the control of probe turning motor with to the control of probe pitching motor, can guarantee to scout probe and can carry out effectively investigation monitoring to ground.
Control system is carried out communication contact, wireless remote control transceiver module and wireless communication module 8 bidirectional wireless communications by wireless communication module 8 and the wireless remote control transceiver module for wireless terminal remote control center personnel,
Wireless remote control transceiver module and wireless communication module 8 wireless telecommunications can realize carries out remote wireless control to reconnaissance flight robot, make reconnaissance flight robot there is intelligent automatic function and artificial remote control function, greatly expanded application scenario and the recon effect of scouting unmanned plane.
The admission direction of video acquisition module 10 and the downrange of Laser emission part 401, the receive direction of laser pick-off part 402 is consistent, the video information that video acquisition module 10 collects sends to wireless remote control control terminal by controller 1 and wireless communication module 8, the operating personal of scouting unmanned plane can be seen the alerting signal of combining of the video information that shows on wireless remote control module 12 and infrared ray and laser intuitively, the direction of video acquisition module 10 and laser ranging is consistent can be so that the video information that video acquisition module 10 collects can be for further confirming the scouting alarming result of infrared ray and laser.
Laser detection module 4 is electrical connected with Laser emission part 401, laser pick-off part 402 respectively, Laser emission part 401 and laser pick-off part 402 be arranged on the first infrared probe 501 and the second infrared probe 502 near; The receive direction of the downrange of the axis of the axis of the first infrared probe 501, the second infrared probe 502 and Laser emission part 401, laser pick-off part 402 all can be positioned at same plane.
Fig. 6 is the structural representation of infrared detection of the present invention, when the first infrared probe 501 and the second infrared probe 502 are set together symmetrically as can be seen from Figure, can obtain extraordinary scouting monitoring effect.The infra-red detection amplitude angle of the first infrared probe 501 is A, and the infra-red detection amplitude angle of the second infrared probe 502 is B, and the distance between the first infrared probe 501 and the second infrared probe 502 is H
1.The infra-red detection amplitude S of the first infrared probe 501
3infra-red detection amplitude S with the second infrared probe 502
4there is region, a blind area S
1, the infra-red detection amplitude S of the first infrared probe 501
3infra-red detection amplitude S with the second infrared probe 502
4there is an overlapping infrared ray overlap-add region S
2, region, blind area S wherein
1axis active distance be H
2, infrared ray overlap-add region S
2axis active distance be H
3, region, blind area S
1with with infrared ray overlap-add region S
2coaxial line, be H
2and H
3coaxial line, region, blind area S
1with with infrared ray overlap-add region S
2axis and the dead ahead of upper scouting probe be consistent, be H
2and H
3be consistent with the investigation dead ahead of scouting probe on flight body.
The first infrared probe 501 and the second infrared probe 502 all can adopt pyroelectric infrared sensor to detect by the infrared signal of scouting personnel or object radiation, at the detector front end formation blind area region S of the first infrared probe 501 and the second infrared probe 502 formation
1with an infrared ray overlap-add region S
2, infrared ray overlap-add region S
2angle C scope be 4-50 degree, infrared ray overlap-add region S
2the preferred 10-20 degree of angle C.That is scouted that infrared ray that object sends just constantly alternately changes enters infrared ray overlap-add region S
2, so just obtained infrared signal with dynamic pulse.By the infrared ray centre wavelength of scouting personnel or object radiation, be 9～10um, on sensor top, offered a window that filter glass is housed, this filter can be 7～10um by light wavelength scope, just in time be suitable for by the detection of scouting personnel or object infrared radiation, and the infrared ray of other wavelength is absorbed by filter.
Infra-ray sensing module 5 is electrical connected with the first infrared probe 501, the second infrared probe 502 respectively, and the first infrared probe 501 and the second infrared probe 502 are arranged on the front end of scouting probe mechanism symmetrically; The infra-red detection amplitude angle A of the first infrared probe 501 is identical with the infra-red detection amplitude angle B of the second infrared probe 502; The infra-red detection region S of the first infrared probe 501
3infra-red detection region S with the second infrared probe 502
4form region, a blind area S
1an and infrared ray overlap-add region S
2.Laser detection module 4 is electrical connected with Laser emission part 401, laser pick-off part 402 respectively, Laser emission part 401 and laser pick-off part 402 be arranged on flight body and with flight body on scout probe investigation forward be consistent.
Claims (6)
1. a scouting unmanned helicopter system, it is characterized in that, comprise controller (1), the first blade group control module (2), the second blade group control module (3), laser detection module (4), infra-ray sensing module (5), probe revolution control module (6), probe pitch control subsystem module (7), wireless communication module (8);
Described controller (1) is electrical connected with described the first blade group control module (2), described the second blade group control module (3), described laser detection module (4), described infra-ray sensing detection module (5), described probe revolution control module (6), described probe pitch control subsystem module (7), described wireless communication module (8) respectively;
Described infra-ray sensing module (5) is electrical connected with the first infrared probe (501), the second infrared probe (502) respectively, and described the first infrared probe (501) and described the second infrared probe (502) are arranged on flight body symmetrically; The infra-red detection amplitude angle A of described the first infrared probe (501) is identical with the infra-red detection amplitude angle B of described the second infrared probe (502); The infra-red detection region S of described the first infrared probe (501)
3infra-red detection region S with described the second infrared probe (502)
4mutually intersect to form an infrared ray blind area region S
1an and infrared ray overlap-add region S
2, described infrared ray overlap-add region S
2angle C, described infrared ray blind area region S
1with described infrared ray overlap-add region S
2coaxially;
Described laser detection module (4) comprises described Laser emission part (401) and described laser pick-off part (402), receive direction and the described infrared ray overlap-add region S of the downrange of described Laser emission part (401), described laser pick-off part (402)
2axis direction in the same way.
2. scouting unmanned helicopter system according to claim 1, is characterized in that, also comprises GPS locating module (9), and described GPS locating module (9) is electrical connected with described controller (1).
3. scouting unmanned helicopter system according to claim 1, is characterized in that, also comprises video acquisition module (10), and described video acquisition module (10) is electrical connected with described controller (1).
4. scouting unmanned helicopter system according to claim 1, is characterized in that, also comprises gyro locating module (11), and described gyro locating module (11) is electrical connected with described controller (1).
5. scouting unmanned helicopter system according to claim 1, it is characterized in that, the receive direction of the admission direction of described video acquisition module (10) and the downrange of described Laser emission part (401), described laser pick-off part (402) is consistent.
6. scouting unmanned helicopter system according to claim 1, is characterized in that, described infrared ray overlap-add region S
2angle C be 4-50 degree.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410182990.5A CN103950536A (en) | 2014-04-30 | 2014-04-30 | Unmanned helicopter system applicable to reconnaissance |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410182990.5A CN103950536A (en) | 2014-04-30 | 2014-04-30 | Unmanned helicopter system applicable to reconnaissance |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN103950536A true CN103950536A (en) | 2014-07-30 |
Family
ID=51327934
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201410182990.5A Pending CN103950536A (en) | 2014-04-30 | 2014-04-30 | Unmanned helicopter system applicable to reconnaissance |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN103950536A (en) |
Cited By (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104515429A (en) * | 2014-12-17 | 2015-04-15 | 蔡德权 | Auxiliary scanning sighting device for assault rifle |
| CN104634174A (en) * | 2014-12-17 | 2015-05-20 | 蔡德权 | Infrared laser auxiliary scanning device for firearm aiming |
| CN104634177A (en) * | 2014-12-17 | 2015-05-20 | 席雅南 | Rifle with target infrared scanning detection device |
| CN104634173A (en) * | 2014-12-17 | 2015-05-20 | 席雅南 | Gun provided with infrared laser auxiliary scanning sighting instrument |
| CN104634175A (en) * | 2014-12-17 | 2015-05-20 | 蔡德权 | Submachine gun target infrared scanning detecting instrument |
| CN104654925A (en) * | 2014-12-17 | 2015-05-27 | 蔡德权 | Submachine gun with assisted infrared laser mixing sighting device |
| CN104654920A (en) * | 2014-12-17 | 2015-05-27 | 席雅南 | Gun provided with infrared laser hybrid assisted sighting device |
| CN105857615A (en) * | 2016-05-16 | 2016-08-17 | 苏州金建达智能科技有限公司 | Unmanned aerial vehicle with object transportation function of robot |
| CN105882967A (en) * | 2016-05-16 | 2016-08-24 | 苏州金建达智能科技有限公司 | Unmanned aerial vehicle device with robot |
| WO2017080109A1 (en) * | 2015-11-14 | 2017-05-18 | 深圳市易特科信息技术有限公司 | Intelligent unmanned aerial vehicle system for remotely detecting target on basis of infrared |
| CN106741888A (en) * | 2017-02-15 | 2017-05-31 | 南京航空航天大学 | A kind of bionical unmanned reconnaissance helicopter |
Citations (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN1768683A (en) * | 2004-10-27 | 2006-05-10 | 三星光州电子株式会社 | Robot cleaner system and a method for returning to external recharging apparatus |
| CN101746503A (en) * | 2008-12-01 | 2010-06-23 | 厦门市罗普特科技有限公司 | Police reconnaissance aircraft with GPS positioning missile |
| CN101811578A (en) * | 2010-04-23 | 2010-08-25 | 福建省电力有限公司福州电业局 | Special photoelectric nacelle of power patrol unmanned helicopter |
| CN101934858A (en) * | 2010-07-08 | 2011-01-05 | 王泽峰 | Miniature electric ducted propeller type intelligent unmanned aerial vehicle |
| CN102414519A (en) * | 2009-04-27 | 2012-04-11 | 日立空调·家用电器株式会社 | Air-conditioner and human body detector thereof |
| CN202264834U (en) * | 2011-10-24 | 2012-06-06 | 常熟理工学院 | Obstacle-surmounting rescue vehicle |
| CN102546689A (en) * | 2010-12-20 | 2012-07-04 | 河南省电力公司驻马店供电公司 | Real-time line walking system of unmanned aerial vehicle |
| CN102749659A (en) * | 2012-07-20 | 2012-10-24 | 湖北久之洋红外系统有限公司 | Multifunctional photoelectric detection instrument and target position observing and determining method implemented by same |
| CN203528816U (en) * | 2013-06-26 | 2014-04-09 | 南昌航空大学 | Aerial photo unmanned plane |
| US8700306B2 (en) * | 2004-06-18 | 2014-04-15 | L-3 Unmanned Systems Inc. | Autonomous collision avoidance system for unmanned aerial vehicles |
-
2014
- 2014-04-30 CN CN201410182990.5A patent/CN103950536A/en active Pending
Patent Citations (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US8700306B2 (en) * | 2004-06-18 | 2014-04-15 | L-3 Unmanned Systems Inc. | Autonomous collision avoidance system for unmanned aerial vehicles |
| CN1768683A (en) * | 2004-10-27 | 2006-05-10 | 三星光州电子株式会社 | Robot cleaner system and a method for returning to external recharging apparatus |
| CN101746503A (en) * | 2008-12-01 | 2010-06-23 | 厦门市罗普特科技有限公司 | Police reconnaissance aircraft with GPS positioning missile |
| CN102414519A (en) * | 2009-04-27 | 2012-04-11 | 日立空调·家用电器株式会社 | Air-conditioner and human body detector thereof |
| CN101811578A (en) * | 2010-04-23 | 2010-08-25 | 福建省电力有限公司福州电业局 | Special photoelectric nacelle of power patrol unmanned helicopter |
| CN101934858A (en) * | 2010-07-08 | 2011-01-05 | 王泽峰 | Miniature electric ducted propeller type intelligent unmanned aerial vehicle |
| CN102546689A (en) * | 2010-12-20 | 2012-07-04 | 河南省电力公司驻马店供电公司 | Real-time line walking system of unmanned aerial vehicle |
| CN202264834U (en) * | 2011-10-24 | 2012-06-06 | 常熟理工学院 | Obstacle-surmounting rescue vehicle |
| CN102749659A (en) * | 2012-07-20 | 2012-10-24 | 湖北久之洋红外系统有限公司 | Multifunctional photoelectric detection instrument and target position observing and determining method implemented by same |
| CN203528816U (en) * | 2013-06-26 | 2014-04-09 | 南昌航空大学 | Aerial photo unmanned plane |
Cited By (14)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104654920A (en) * | 2014-12-17 | 2015-05-27 | 席雅南 | Gun provided with infrared laser hybrid assisted sighting device |
| CN104515429A (en) * | 2014-12-17 | 2015-04-15 | 蔡德权 | Auxiliary scanning sighting device for assault rifle |
| CN104634177A (en) * | 2014-12-17 | 2015-05-20 | 席雅南 | Rifle with target infrared scanning detection device |
| CN104634173A (en) * | 2014-12-17 | 2015-05-20 | 席雅南 | Gun provided with infrared laser auxiliary scanning sighting instrument |
| CN104634175A (en) * | 2014-12-17 | 2015-05-20 | 蔡德权 | Submachine gun target infrared scanning detecting instrument |
| CN104654925A (en) * | 2014-12-17 | 2015-05-27 | 蔡德权 | Submachine gun with assisted infrared laser mixing sighting device |
| CN104634174A (en) * | 2014-12-17 | 2015-05-20 | 蔡德权 | Infrared laser auxiliary scanning device for firearm aiming |
| WO2017080109A1 (en) * | 2015-11-14 | 2017-05-18 | 深圳市易特科信息技术有限公司 | Intelligent unmanned aerial vehicle system for remotely detecting target on basis of infrared |
| CN105857615A (en) * | 2016-05-16 | 2016-08-17 | 苏州金建达智能科技有限公司 | Unmanned aerial vehicle with object transportation function of robot |
| CN105882967A (en) * | 2016-05-16 | 2016-08-24 | 苏州金建达智能科技有限公司 | Unmanned aerial vehicle device with robot |
| CN105882967B (en) * | 2016-05-16 | 2018-12-21 | 南京国器智能装备有限公司 | A kind of unmanned plane device with robot |
| CN105857615B (en) * | 2016-05-16 | 2019-01-15 | 深圳市星睿达科技有限公司 | A kind of unmanned plane with robotic article transportation function |
| CN106741888A (en) * | 2017-02-15 | 2017-05-31 | 南京航空航天大学 | A kind of bionical unmanned reconnaissance helicopter |
| CN106741888B (en) * | 2017-02-15 | 2023-09-26 | 南京航空航天大学 | Bionic unmanned reconnaissance helicopter |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN103950536A (en) | Unmanned helicopter system applicable to reconnaissance | |
| CN103963968A (en) | Remotely-controlled unmanned helicopter reconnaissance system | |
| KR101881396B1 (en) | System for cooperative anti-drone and method for cooperation control of anti-drones | |
| CN111664752B (en) | Unmanned aerial vehicle counter-braking system | |
| US8573529B2 (en) | Standoff detection of motion and concealed unexploded ordnance (UXO) | |
| WO2018036323A1 (en) | Defense system and method for defending against low-flying unmanned aerial vehicle | |
| CN203819497U (en) | Fire-fighting unmanned aerial vehicle system based on 3G network | |
| CN110624189B (en) | Unmanned aerial vehicle-mounted fire extinguishing bomb device, fire-fighting unmanned aerial vehicle and emission control method | |
| KR20190097624A (en) | Anti-Drones system and operation methode to neutralize abusing drones | |
| CN205525015U (en) | Multi -functional firefighting rescue unmanned aerial vehicle | |
| CN201334116Y (en) | Hovering police reconnaissance flight vehicle with infra-red range measuring function | |
| CN204846371U (en) | Can keep away unmanned aerial vehicle system of barrier | |
| CN202267872U (en) | Sensitive unmanned helicopter system | |
| CN209392631U (en) | A kind of high-altitude unmanned plane and fire-extinguishing | |
| CN105509554A (en) | Shoot robot equipped with infrared-ultrasonic mixed aiming device | |
| CN105423817A (en) | Shooting robot provided with infrared and ultrasonic mixed auxiliary aiming device | |
| CN107008017B (en) | A kind of dedicated multifunction detecting dummy vehicle of teenager's defence education | |
| KR20190097609A (en) | Drone for overpowering the criminals | |
| Kadıoğlu et al. | Development of unmanned aerial vehicle for detecting the forest fires | |
| CN204229577U (en) | Based on the firefighting monitoring system of fire analysis | |
| CN216684840U (en) | Trapped person search and rescue system based on millimeter wave radar | |
| CN105423820A (en) | Infrared laser mixed aiming anti-terrorist robot | |
| Zhao et al. | Design of Intelligent Flight Platform for High-Rise Fire Fighting and Rescue | |
| CN105500329A (en) | Infrared-ultrasonic mixed aiming shoot robot | |
| CN105509561A (en) | Infrared-ultrasonic mixed aiming-assisted counter-terrorism robot |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| C02 | Deemed withdrawal of patent application after publication (patent law 2001) | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20140730 |