CN104503458A - Micro individual combat unmanned plane system - Google Patents
Micro individual combat unmanned plane system Download PDFInfo
- Publication number
- CN104503458A CN104503458A CN201410652488.6A CN201410652488A CN104503458A CN 104503458 A CN104503458 A CN 104503458A CN 201410652488 A CN201410652488 A CN 201410652488A CN 104503458 A CN104503458 A CN 104503458A
- Authority
- CN
- China
- Prior art keywords
- aircraft
- helmet
- individual soldier
- wing
- individual
- 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
- Helmets And Other Head Coverings (AREA)
Abstract
The invention relates to a micro individual combat unmanned plane system. The micro individual combat unmanned plane system comprises an aircraft, a hand-held controller and an individual helmet, wherein the aircraft is equipped with airborne communication equipment, an airborne controller and airborne task equipment, the aircraft and the hand-held controller are in wireless connection through wireless communication equipment, and the aircraft and the individual helmet are in wireless connection through wireless communication equipment. The micro individual combat unmanned plane system has advantages of excellent pneumatic layout, excellent self stability, high security, strong outfield maintenance capability, convenient carrying, simple operation and short start preparation time.
Description
Technical field
The invention belongs to unmanned plane field, especially a kind of small-sized individual combat UAS.
Background technology
In recent years, along with the maturation gradually of unmanned spacecraft technology, and the progress of supporting opertaing device had possessed the feasibility of technical multiple application.Current UAS is normally undertaken unifying to control by ground control station, and single unmanned plane application of going out when executing the task comparatively is short of, and dirigibility is not enough.
Do not find the publication technology identical with this patent through preliminary search, and not yet occur similar products in my home market at present according to research.
Summary of the invention
The object of the invention is to overcome the deficiencies in the prior art part, a kind of small-sized individual combat UAS is provided.
The present invention solves its technical matters and takes following technical scheme to realize:
A kind of small-sized individual combat UAS, it is characterized in that: comprise aircraft, hand held controller and individual soldier's helmet, aircraft is provided with airborne communication control, on-board controller and airborne task device, wireless connections are carried out by Wireless Telecom Equipment between aircraft and hand held controller, wireless connections are carried out by Wireless Telecom Equipment between aircraft and individual soldier's helmet
(1) concrete structure of aircraft, adopt carbon fibre composite to make, comprise fuselage, main wing, flank, screw propeller and motor, the equal symmetrical elasticity of this fuselage both lateral sides is hinged with a wing, is hinged with flank outside wing, and fuselage and wing are 5 sections; In the middle part of the main wing of these aircraft both sides, front end is separately installed with one by the screw propeller of drive and control of electric machine, and the motor of these both sides is controlled respectively by on-board controller; Screw propeller adopts soft folding screw wing, Automatic-expanding during rotation; Airborne task device is installed in aircraft lower end;
(2) system of hand held controller is that JAUS is compatible, is based on high stability (SuSE) Linux OS;
(3) individual soldier's helmet comprises individual soldier's signal transmission apparatus, processing signals converter, storer, individual soldier's signal converter, video player, image scanning module, audio-frequency module and distance-measuring device, the front end of the helmet is provided with camera by angle controller, the helmet is anterior by support hinge dress video player, the inside of helmet both sides is provided with audio-frequency module, this audio-frequency module comprises microphone and earphone, helmet rear end is fixed with a control enclosure, individual soldier's signal transmission apparatus is installed in this control enclosure, processing signals converter, storer, individual soldier's signal converter and distance-measuring device.
And described airborne task device is photoelectric nacelle, comprises thermal camera, visible light camera and range finder using laser.
And described airborne task device is thermal camera.
Advantage of the present invention and good effect are:
1, the present invention possesses and vertical takeoff and landing, hand can throw and fly, parachuting, hit the multiple landing modes such as net landing, and have lightweight, collapsible, easy to carry, simple operation and other advantages, easy to carry, individual soldier can carry 2-4 piece of CD-1UAV.
2, real-time high definition image transmission of the present invention, 12 Zoom Lens, scouting, precision strike, incidentally few advantage is injured.
3, aerodynamic arrangement of the present invention is good, and self stability is excellent, and security is high; Flight-line service ability is strong, is easy to carry; Simple to operate, start setup time short.
Accompanying drawing explanation
Fig. 1 is system chart of the present invention;
Fig. 2 is the structural front view of aircraft;
Fig. 3 is the vertical view of Fig. 2;
Fig. 4 is the structural representation of individual soldier's helmet.
Embodiment
Below in conjunction with accompanying drawing, also by specific embodiment, the invention will be further described, and following examples are descriptive, are not determinate, can not limit protection scope of the present invention with this.
A kind of small-sized individual combat UAS, comprise aircraft, hand held controller and individual soldier's helmet, aircraft is provided with airborne communication control, on-board controller and airborne task device, carry out wireless connections by Wireless Telecom Equipment between aircraft and hand held controller, between aircraft and individual soldier's helmet, carry out wireless connections by Wireless Telecom Equipment.
(1) concrete structure of aircraft is see accompanying drawing 2 and accompanying drawing 3, adopts carbon fibre composite to make, has lightweight feature, can improve load; Comprise fuselage 1, main wing 3, flank 4, screw propeller 2 and motor 5, the equal symmetrical elasticity of this fuselage both lateral sides is hinged with a wing, is hinged with flank outside wing, fuselage and wing are 5 sections, when carrying, the wing of both sides is carried out the folding length that can make and reduce 60%, compact, portable;
In the middle part of the main wing of these aircraft both sides, front end is separately installed with one by the screw propeller of motor 5 drived control, and the motor of these both sides is controlled respectively by on-board controller, motor speed adjustable, can adapt to wider velocity range; Screw propeller adopts soft folding screw wing, and Automatic-expanding during rotation, can not injure wing.
This vehicle technology parameter
Operational distance: 5-10km
CD-1 size: 50*200*620
The span: 1.4m
Operation flight relative height: 50m ~ 1000m
Payload capacity: 0.5kg
Velocity range: 45 ~ 120km/h (sea-level standard air)
Propulsion system: brushless motor two
Cruise speed: 80km/h
Cruise time: 50 scout; Hit 20
Maximum take-off weight: 1500g
Wind loading rating: 4 grades of vertical takeoff and landing, 6 grades are cruised
Airborne task device is installed in aircraft lower end, and the airborne task device of the present embodiment adopts modular design, and be convenient to change, the present embodiment selects following equipment:
1. photoelectric nacelle is a kind of optical device applying gyrocontrol technology; Generally include the multiple optical sensors such as thermal camera, visible light camera and range finder using laser, and there is the function of isolation carrier movement maintenance boresight at inertial space angle stabilization; The various carrying platforms such as helicopter, fixed wing aircraft, unmanned plane, naval vessel and vehicle can be equipped on; Can be used for the military fields such as scouting, aiming, missile guidance, also can be used for the non-military fields such as search and rescue, anti-smuggling, safety, environmental monitoring, forest fire protection.Photoelectric nacelle feature: adopt biaxial stabilization platform, volume is little, lightweight; Adopt low-cost design, the tasks such as forest fire protection, search and rescue, anti-smuggling can be completed; Highgrade integration designs, and control circuit is built-in; Be applicable to the airborne application such as unmanned plane, light aerocraft.
2. thermal camera, visible light camera, ensures to gather image identical with the visible image of human eye;
(2) the system JAUS of hand held controller is compatible, is based on high stability (SuSE) Linux OS, adopts advanced control technology, can be more natural, intuitively, realizes the interaction between people and aircraft;
(3) individual soldier's helmet structure figure is see accompanying drawing 1 and accompanying drawing 4, comprise individual soldier's signal transmission apparatus, processing signals converter, storer, individual soldier's signal converter, video player, image scanning module, audio-frequency module and distance-measuring device, the front end of the helmet 11 is provided with camera 7 by angle controller 8, the helmet is anterior by support hinge dress video player 6, the inside of helmet both sides is provided with audio-frequency module, this audio-frequency module comprises microphone 9 and earphone 10, helmet rear end is fixed with a control enclosure 12, individual soldier's signal transmission apparatus is installed in this control enclosure, processing signals converter, storer, individual soldier's signal converter and distance-measuring device.
Individual soldier's helmet can promote the perception of soldier, help they around environment occur variation time, make adjustment rapidly and dispose.On battlefield, the map etc. in the position of such as enemy army, the orientation of comrade-in-arms and city or house is all the utilizable important information of soldier.The visual helmet of individual soldier arises at the historic moment thus, and it can measuring distance, scans the 3D rendering of building, can also the video that gathers of real-time Transmission unmanned plane.
In addition, it is also furnished with the function of night vision enhancing and enemy and we's identification.The real time data beyond visual range can be collected and provide text message, warning and threat etc. to soldier.Had the help of these information, soldier will obtain additional advantage at reply dangerous situation.
Communication facilities: body always has two antennas, is respectively Data-Link antenna and lower Data-Link antenna.Uplink is responsible for receiving instruction, and lower link is responsible for the information such as transmission of video information, video tracking state, flight parameter.
Transmission of video flow process is introduced: by the high definition Image transmission equipment of aircraft by vision signal real-time Transmission to terrestrial operation device, then by terrestrial operation device, control task order has been reached instruction.
The application of native system
(1) military requirement
When performing combat duty, when not exposing own target, enemy's trend can be grasped, guided by operator, adopt television guided mode offensive attack, accurately rush at target, and blasting in a flash of target can clashed into, or realize type self-destroyed blast when target run overhead.
Look into dozen unmanned plane and can carry high explosive, target can be eliminated rapidly after ignition, can enemy firepower be slackened, as sniper, machine gunner, and mortar etc.
(2) application is scouted
Look into that to beat be aly by electronic reconnaissance equipment on machine, to obtain the UAS of target information, can may be used for battlefield surveillance, for the operation of army provides intelligence, information can be divided into, strategfic reconnaissance, the reconnaissance of a campaign nature and tactical reconnaissance.
(3) application is hit
When performing combat duty, when not exposing own target, enemy's trend can be grasped, guided by operator, adopt television guided mode offensive attack, accurately rush at target, and blasting in a flash of target can clashed into, or realize type self-destroyed blast when target run overhead.
Look into dozen unmanned plane and can carry high explosive, target can be eliminated rapidly after ignition, can enemy firepower be slackened, as sniper, machine gunner, and mortar etc.
Although disclose embodiments of the invention and accompanying drawing for the purpose of illustration, but it will be appreciated by those skilled in the art that: in the spirit and scope not departing from the present invention and claims, various replacement, change and amendment are all possible, therefore, scope of the present invention is not limited to the content disclosed in embodiment and accompanying drawing.
Claims (3)
1. a small-sized individual combat UAS, it is characterized in that: comprise aircraft, hand held controller and individual soldier's helmet, aircraft is provided with airborne communication control, on-board controller and airborne task device, carry out wireless connections by Wireless Telecom Equipment between aircraft and hand held controller, between aircraft and individual soldier's helmet, carry out wireless connections by Wireless Telecom Equipment;
(1) concrete structure of aircraft, adopt carbon fibre composite to make, comprise fuselage, main wing, flank, screw propeller and motor, the equal symmetrical elasticity of this fuselage both lateral sides is hinged with a wing, is hinged with flank outside wing, and fuselage and wing are 5 sections; In the middle part of the main wing of these aircraft both sides, front end is separately installed with one by the screw propeller of drive and control of electric machine, and the motor of these both sides is controlled respectively by on-board controller; Screw propeller adopts soft folding screw wing, Automatic-expanding during rotation; Airborne task device is installed in aircraft lower end;
(2) system of hand held controller is that JAUS is compatible, is based on high stability (SuSE) Linux OS;
(3) individual soldier's helmet comprises individual soldier's signal transmission apparatus, processing signals converter, storer, individual soldier's signal converter, video player, image scanning module, audio-frequency module and distance-measuring device, the front end of the helmet is provided with camera by angle controller, the helmet is anterior by support hinge dress video player, the inside of helmet both sides is provided with audio-frequency module, this audio-frequency module comprises microphone and earphone, helmet rear end is fixed with a control enclosure, individual soldier's signal transmission apparatus is installed in this control enclosure, processing signals converter, storer, individual soldier's signal converter and distance-measuring device.
2. small-sized individual combat UAS according to claim 1, is characterized in that: described airborne task device is photoelectric nacelle, comprises thermal camera, visible light camera and range finder using laser.
3. small-sized individual combat UAS according to claim 1, is characterized in that: described airborne task device is thermal camera.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410652488.6A CN104503458A (en) | 2014-11-17 | 2014-11-17 | Micro individual combat unmanned plane system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410652488.6A CN104503458A (en) | 2014-11-17 | 2014-11-17 | Micro individual combat unmanned plane system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN104503458A true CN104503458A (en) | 2015-04-08 |
Family
ID=52944862
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201410652488.6A Pending CN104503458A (en) | 2014-11-17 | 2014-11-17 | Micro individual combat unmanned plane system |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN104503458A (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106767211A (en) * | 2017-01-11 | 2017-05-31 | 中南大学 | A kind of Pass blocks demolition set and method |
| CN106963019A (en) * | 2017-04-25 | 2017-07-21 | 苏州科伊嘉航空科技有限公司 | A kind of day eye Hull-Mounted Set |
| CN107063471A (en) * | 2017-05-12 | 2017-08-18 | 凯迈（洛阳）测控有限公司 | Individual soldier based on MEMS infrared light supplies recognizes the helmet with radio recognition equipment, enemy and we |
| CN109916227A (en) * | 2017-12-13 | 2019-06-21 | 中电科特种飞机系统工程有限公司 | A kind of anti-unmanned aerial vehicle control system and method |
| CN112817322A (en) * | 2020-12-31 | 2021-05-18 | 珠海紫燕无人飞行器有限公司 | Head-mounted unmanned helicopter control system and control method thereof |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE19731724A1 (en) * | 1997-07-23 | 1999-01-28 | Horst Juergen Dipl Ing Duschek | Virtual reality control method for unmanned helicopter, aircraft etc. |
| CN200944156Y (en) * | 2006-06-19 | 2007-09-05 | 天津大学 | Wearing appliance for monitoring unmanned aircraft |
| CN102591346A (en) * | 2011-12-05 | 2012-07-18 | 大连理工大学 | Small-size handheld ground monitoring system for unmanned aerial vehicle |
| CN203193785U (en) * | 2012-12-14 | 2013-09-11 | 国家电网公司 | Glasses |
| CN203759525U (en) * | 2014-03-26 | 2014-08-06 | 朱奇 | Digital remote control system based on tablet PC |
-
2014
- 2014-11-17 CN CN201410652488.6A patent/CN104503458A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE19731724A1 (en) * | 1997-07-23 | 1999-01-28 | Horst Juergen Dipl Ing Duschek | Virtual reality control method for unmanned helicopter, aircraft etc. |
| CN200944156Y (en) * | 2006-06-19 | 2007-09-05 | 天津大学 | Wearing appliance for monitoring unmanned aircraft |
| CN102591346A (en) * | 2011-12-05 | 2012-07-18 | 大连理工大学 | Small-size handheld ground monitoring system for unmanned aerial vehicle |
| CN203193785U (en) * | 2012-12-14 | 2013-09-11 | 国家电网公司 | Glasses |
| CN203759525U (en) * | 2014-03-26 | 2014-08-06 | 朱奇 | Digital remote control system based on tablet PC |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106767211A (en) * | 2017-01-11 | 2017-05-31 | 中南大学 | A kind of Pass blocks demolition set and method |
| CN106767211B (en) * | 2017-01-11 | 2018-08-14 | 中南大学 | A kind of Pass blocks demolition set and method |
| CN106963019A (en) * | 2017-04-25 | 2017-07-21 | 苏州科伊嘉航空科技有限公司 | A kind of day eye Hull-Mounted Set |
| CN107063471A (en) * | 2017-05-12 | 2017-08-18 | 凯迈（洛阳）测控有限公司 | Individual soldier based on MEMS infrared light supplies recognizes the helmet with radio recognition equipment, enemy and we |
| CN109916227A (en) * | 2017-12-13 | 2019-06-21 | 中电科特种飞机系统工程有限公司 | A kind of anti-unmanned aerial vehicle control system and method |
| CN112817322A (en) * | 2020-12-31 | 2021-05-18 | 珠海紫燕无人飞行器有限公司 | Head-mounted unmanned helicopter control system and control method thereof |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| KR102600479B1 (en) | Aerial vehicle interception system | |
| JP7207897B2 (en) | Imaging and targeting systems for air vehicles | |
| US11074827B2 (en) | Virtual reality system for aerial vehicle | |
| CN104503458A (en) | Micro individual combat unmanned plane system | |
| US9725172B2 (en) | Surveillance system | |
| US20110186687A1 (en) | Unmanned gyrokite as self-powered airborne platform for electronic systems | |
| CN204822083U (en) | For military use alert unmanned aerial vehicle system that uses of multipurpose | |
| CN105573343A (en) | Capture system based on unmanned aerial vehicle | |
| CN107140209A (en) | A kind of unmanned plane targeted system | |
| US11097840B2 (en) | Anti-personnel autonomous vehicle | |
| KR20150120401A (en) | Vertical take off and landing unmanned aerial vehicle with twin yaw control system | |
| RU82674U1 (en) | UNMANNED AIRCRAFT HELICOPTER TYPE | |
| JP2022521523A (en) | Weapon targeting training system and its methods | |
| CN204270148U (en) | A kind of small-sized individual combat UAS | |
| WO2011144497A1 (en) | Remotely operated air reconnaissance device | |
| CN204606206U (en) | Dazzle the eyes TUAV | |
| CN218806669U (en) | Low-slow small target reconnaissance countercheck system based on multi-rotor unmanned aerial vehicle | |
| CN207417153U (en) | It is a kind of can anticollision Intelligent unattended machine | |
| CN114987777A (en) | Low-slow small target reconnaissance and countercheck system and method based on multi-rotor unmanned aerial vehicle | |
| CN204433032U (en) | A kind of portable small-sized individual combat aircraft | |
| CN110645834A (en) | Intelligent wushu ware station control system | |
| Pilch et al. | Survey of the status of small armed and unarmed uninhabited aircraft | |
| RU2742495C2 (en) | Multifunctional aerodynamic distributed system | |
| RU2812501C1 (en) | Method of preparing remote combat operations | |
| Heichal | Importance of Unmanned Air Vehicles |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20150408 |
|
| RJ01 | Rejection of invention patent application after publication |