CN106043693A - Unmanned aerial vehicle for surveying and mapping - Google Patents
Unmanned aerial vehicle for surveying and mapping Download PDFInfo
- Publication number
- CN106043693A CN106043693A CN201610414299.4A CN201610414299A CN106043693A CN 106043693 A CN106043693 A CN 106043693A CN 201610414299 A CN201610414299 A CN 201610414299A CN 106043693 A CN106043693 A CN 106043693A
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- China
- Prior art keywords
- mapping
- unmanned plane
- surveying
- aerial vehicle
- unmanned aerial
- 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.)
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- 238000013507 mapping Methods 0.000 title claims abstract description 41
- 238000000034 method Methods 0.000 claims description 14
- 230000004297 night vision Effects 0.000 claims description 7
- 230000005540 biological transmission Effects 0.000 claims description 4
- WHXSMMKQMYFTQS-UHFFFAOYSA-N Lithium Chemical group [Li] WHXSMMKQMYFTQS-UHFFFAOYSA-N 0.000 claims description 3
- 230000001133 acceleration Effects 0.000 claims description 3
- 238000001914 filtration Methods 0.000 claims description 3
- 229910052744 lithium Inorganic materials 0.000 claims description 3
- 239000004033 plastic Substances 0.000 claims description 3
- 229920003023 plastic Polymers 0.000 claims description 3
- 239000000284 extract Substances 0.000 claims description 2
- 230000005611 electricity Effects 0.000 claims 1
- 230000007613 environmental effect Effects 0.000 abstract description 3
- 238000012544 monitoring process Methods 0.000 abstract description 3
- 238000005259 measurement Methods 0.000 abstract description 2
- 238000011156 evaluation Methods 0.000 abstract 2
- 238000004891 communication Methods 0.000 abstract 1
- 230000000694 effects Effects 0.000 abstract 1
- 230000002035 prolonged effect Effects 0.000 abstract 1
- 238000010276 construction Methods 0.000 description 3
- 238000005516 engineering process Methods 0.000 description 3
- 208000035473 Communicable disease Diseases 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000003139 buffering effect Effects 0.000 description 1
- 238000012937 correction Methods 0.000 description 1
- 230000007123 defense Effects 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 238000000605 extraction Methods 0.000 description 1
- 238000003384 imaging method Methods 0.000 description 1
- 208000015181 infectious disease Diseases 0.000 description 1
- 238000007689 inspection Methods 0.000 description 1
- 238000007726 management method Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000011084 recovery Methods 0.000 description 1
- 238000012876 topography Methods 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/25—Fixed-wing aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2101/00—UAVs specially adapted for particular uses or applications
- B64U2101/30—UAVs specially adapted for particular uses or applications for imaging, photography or videography
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2201/00—UAVs characterised by their flight controls
- B64U2201/10—UAVs characterised by their flight controls autonomous, i.e. by navigating independently from ground or air stations, e.g. by using inertial navigation systems [INS]
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Remote Sensing (AREA)
- Position Fixing By Use Of Radio Waves (AREA)
Abstract
The invention relates to the field of unmanned aerial vehicle surveying and mapping, in particular to an unmanned aerial vehicle for surveying and mapping. The problems of using limitation, function simplicity and the like in the prior art are solved. The unmanned aerial vehicle for surveying and mapping is invented for meeting the requirements for disaster evaluation, emergency monitoring, geographical mapping, environmental evaluation and the like. The unmanned aerial vehicle for surveying and mapping has the multiple functions of surveying, mapping, communication, rescuing, data forwarding, power generating and the like, and the functions are complete; measurement of multiple data can be achieved at the same time; a solar power generating device is arranged, the overall working time of the unmanned aerial vehicle is prolonged, and the energy-saving environment-friendly effect is achieved. The unmanned aerial vehicle has the characteristics of being portable, easy to maintain and use, low in cost, reusable and the like, has wide market demand and is easy to apply and popularize.
Description
Technical field
The present invention relates to unmanned plane survey field, be specially one mapping unmanned plane.
Background technology
Mapping science is widely used in economic construction and national defense construction.Rural and urban construction plans, land resources utilize,
In the work such as environmental conservation, it is necessary to carry out land survey and survey and draw various maps, for planning and management.
Unmanned plane presses application, can be divided into military and civilian.Military aspect, unmanned plane is divided into reconnaissance plane and target drone.The people
With aspect, unmanned plane+sector application, it is real just the needing of unmanned plane；At present taking photo by plane, agricultural, plant protection, auto heterodyne, express transportation,
Disaster relief, observation wild animal, monitoring infectious disease, mapping, news report, electric inspection process, the disaster relief, movies-making, manufacture wave
The application in unrestrained etc. field, has greatly expanded the purposes of unmanned plane itself, developed country also in actively extension sector application and
Development unmanned air vehicle technique, unmanned plane not only can complete the task that manned aircraft performs, and being more suitable for people's aircraft should not hold
The task of row.
Current most photogrammetric state, zonule high accuracy topography mapping, depend on the people in field always
Work operating type.As the lifting of tradition airborne and spaceborne RS means, unmanned plane surveying and mapping technology becomes study hotspot.Current
Unmanned aerial vehicle is for different mission requirementses and uses condition difference very big, and mostly carries and use inconvenience, relatively costly.
In patent database, retrieval to the patent of aircraft survey field be all similar to camera function, and transmission performance
Poor and function singleness problem.
Summary of the invention
The present invention is directed to problem present in above-mentioned technology, it is provided that a kind of mapping unmanned plane, solve in prior art
There is the problem such as limitation, function singleness of use.
To achieve these goals, technical scheme is as follows:
A kind of mapping unmanned plane, comprising: body, nose-gear, rear undercarriage, wing, propeller, empennage, infrared ray
Range unit, motor, battery, radio receiver-transmitter, night-vision devices, automatic pilot, surveying and mapping tool cabin, GPS positioner,
Accumulator apparatus, rudder, umbrella cabin, solar panel.
Described underpart front end is provided with undercarriage and rear portion is provided with rear undercarriage, and described body connects wing, institute
Stating empennage and be installed on the afterbody of body, described motor apparatus is in the inside of front part of a body, and described motor is connected to propeller, described
Infrared distance measuring device is installed on the outside of body front end, and described battery is arranged in the lower space of body, described radio
R-T unit is installed on the upper ends of body, and described night-vision devices are installed on the upper bit of body front end infrared distance measuring device
Putting, described automatic pilot is installed on internal body wing lower position, and described surveying and mapping tool cabin and GPS positioner are installed on
Position in the middle of body, described storage device installs the afterbody of wing, and described umbrella cabin is installed on the top of body front end, described too
Sun energy panel is installed on the position after the wing of body outer top, and described rudder is installed on empennage top.
Described propeller is plastics constant pitch airscrew.
Described motor is electro-motor.
Described battery is lithium battery.
Described surveying and mapping tool cabin includes: height above sea level instrument, camera head, two-dimensional scanner, wherein said two-dimensional scan
Device is photogrammetry device.
Described accumulator apparatus includes: controller, processor.
Described rudder includes: turn to rudder, elevator.
Described automatic pilot possesses automatic Pilot and Autonomous Control unmanned plane function, uses PID control method, passes through
The Kalman filtering revised with GPS carries out data resolving, and the remote information that come by data link transmission also extracts correct
Control signal, to 3 to acceleration, 3 fly to the reconnaissance platforms of gyro data acquisition process, baroceptor and navigator collection
Data during row are received；In unmanned plane take-off process, Autonomous Control unmanned aerial vehicle ejecting takes off, in flight course
Route task according to planning in advance processes, and sends instruction to actuator, controls actuator and performs corresponding task, and
Can need to carry out in real time change and the planning of flight path route according to actual task.
Beneficial effects of the present invention: the present invention be directed to the sides such as the condition of a disaster assessment, emergency monitoring, geographical mapping, environmental assessment
A kind of mapping unmanned plane that the demand in face is developed.Have mapping, communicate, rescue, data forwarding, the multiple function such as generating, function is neat
Entirely；The measurement of multiple data can be realized simultaneously；Configuration device of solar generating, extends the working time of integral device, energy-saving ring
Protect.Have easy to carry, safeguard and use simple, low cost, the feature such as reusable have the wide market demand, it is easy to
Popularization and application.
Accompanying drawing explanation
Fig. 1 is the structural representation of the present invention.
Detailed description of the invention
It is an object of the invention to provide a kind of mapping unmanned plane, solved and prior art exists use limitation, merit
The problems such as energy unicity.
To achieve these goals, technical scheme is as follows:
Shown in Fig. 1, a kind of mapping unmanned plane, comprising: body 1, nose-gear 2, rear undercarriage 3, wing 4, spiral
Oar 5, empennage 6, infrared distance measuring device 7, motor 8, battery 9, radio receiver-transmitter 10, night-vision devices 11, automatic pilot
12, surveying and mapping tool cabin 13, GPS positioner 14, accumulator apparatus 15, rudder 16, umbrella cabin 17, solar panel 18.
Described body 1 lower front part is provided with undercarriage 2 and rear portion is provided with rear undercarriage 3, and described body connects wing
4, described empennage 6 is installed on the afterbody of body 1, and described motor 8 is installed on the inside of body 1 front portion, and described motor 8 is connected to spiral shell
Rotation oar 5, described infrared distance measuring device 7 is installed on the outside of body 1 front end, and described battery 9 is arranged at the lower space of body 1
In, described radio receiver-transmitter 10 is installed on the upper ends of body 1, and it is red that described night-vision devices 11 are installed on body 1 front end
The upper position of outside line range unit 7, described automatic pilot 12 is installed on body 1 inner airfoil 4 lower position, described mapping
Instrument cabin 13 and GPS positioner 14 is installed on the position in the middle of body 1, and described storage device 15 installs the afterbody of wing 4, institute
Stating umbrella cabin 17 and be installed on the top of body 1 front end, described solar panel 18 is installed on the position after body 1 outer top wing 4,
Described rudder 16 is installed on empennage 6 top.
Described propeller 5 is preferably plastics constant pitch airscrew.
Described motor 8 is preferably electro-motor.
Described battery 9 is preferably lithium battery.
Described surveying and mapping tool cabin 13 includes: height above sea level instrument, camera head, two-dimensional scanner, and wherein said two dimension is swept
Imaging apparatus is photogrammetry device.
Described accumulator apparatus 11 includes: controller, processor.
Described rudder 16 includes: turn to rudder, elevator.
Described automatic pilot 12 possesses automatic Pilot and Autonomous Control unmanned plane function, uses PID control method, logical
The Kalman filtering crossing band GPS correction carries out data resolving, and the remote information the extraction that are come by data link transmission are correct
Control signal, to 3 to acceleration, 3 to gyro data acquisition process, baroceptor and navigator gather reconnaissance platforms
Data in flight course are received；In unmanned plane take-off process, Autonomous Control unmanned aerial vehicle ejecting takes off, at flight course
The route task that middle basis is planned in advance processes, and sends instruction to actuator, controls actuator and performs corresponding task,
And can need to carry out in real time change and the planning of flight path route according to actual task.
Operation principle
Customized type course line can be set for mapping coverage, make unmanned plane take photo by plane accordingly according to predetermined course line or navigate
Take the photograph.Recovery can use automatic deployment mode, uses the way point of automatic pilot to arrange in advance, can be set as arriving set point
Coordinate i.e. releases a parachute and simultaneously closes off motor, is carried out buffering subtracted by undercarriage and three rubber wheels during undercarriage landing
Shake, completes aircraft by skidding and grounds.Each device collaborative work, make the surveying and mapping tool in surveying and mapping tool cabin, night-vision devices, from
Dynamic pilot, GPS positioner, accumulator apparatus, infrared distance measuring device, radio receiver-transmitter have mapping, communicate, rescue
Help, data forward, etc. multiple function.
The invention is not restricted to the details of above-mentioned one exemplary embodiment, and in the spirit or essential attributes without departing substantially from the present invention
In the case of, it is possible to realize the present invention in other specific forms.Which point therefore, no matter from the point of view of, embodiment all should be seen
Work is exemplary, and is nonrestrictive, and those skilled in the art should be using description as an entirety, each embodiment
In technical scheme can also form other embodiments that it will be appreciated by those skilled in the art that, the present invention through appropriately combined
Scope limited by claims rather than described above, it is intended that by the implication of equivalency in claim that falls
Include in the present invention with all changes in scope.
Claims (7)
1. a mapping unmanned plane, it is characterised in that comprising: body, nose-gear, rear undercarriage, wing, propeller, tail
The wing, infrared distance measuring device, motor, battery, radio receiver-transmitter, night-vision devices, automatic pilot, surveying and mapping tool cabin, GPS
Positioner, accumulator apparatus, rudder, umbrella cabin, solar panel；Wherein, described underpart front end be provided with undercarriage and after
Portion is provided with rear undercarriage, and described body connects wing, and described empennage is installed on the afterbody of body, and described motor apparatus is in body
Anterior inside, described motor is connected to propeller, and described infrared distance measuring device is installed on the outside of body front end, described electricity
Pond is arranged in the lower space of body, and described radio receiver-transmitter is installed on the upper ends of body, described night-vision devices
Being installed on the upper position of body front end infrared distance measuring device, described automatic pilot is installed on orientation under internal body wing
Putting, described surveying and mapping tool cabin and GPS positioner are installed on the position in the middle of body, and described storage device installs the tail of wing
Portion, described umbrella cabin is installed on the top of body front end, and described solar panel is installed on the position after the wing of body outer top, institute
State rudder and be installed on empennage top.
A kind of mapping unmanned plane the most according to claim 1, it is characterised in that determine comprising: described propeller is plastics
Away from propeller.
A kind of mapping unmanned plane the most according to claim 1, it is characterised in that comprising: described motor is electro-motor.
A kind of mapping unmanned plane the most according to claim 1, it is characterised in that comprising: described battery is lithium battery.
A kind of mapping unmanned plane according to claim 1, it is characterised in that comprising: described surveying and mapping tool cabin includes: sea
Pulling out altimeter, camera head, two-dimensional scanner, wherein said two-dimensional scanner is photogrammetry device.
A kind of mapping unmanned plane the most according to claim 1, it is characterised in that comprising: described accumulator apparatus includes:
Controller, processor.
A kind of mapping unmanned plane the most according to claim 1, it is characterised in that comprising: described rudder includes: turn to rudder,
Elevator.
A kind of mapping unmanned plane the most according to claim 1, it is characterised in that comprising: described automatic pilot tool
Standby automatic Pilot and Autonomous Control unmanned plane function, use PID control method, and the Kalman filtering revised by band GPS is carried out
Data resolve, and the remote information that come by data link transmission also extracts correct control signal, to 3 to acceleration, 3 to top
Data in the reconnaissance platforms flight course of spiral shell data acquisition process, baroceptor and navigator collection are received；?
In unmanned plane take-off process, Autonomous Control unmanned aerial vehicle ejecting takes off, and enters according to the route task planned in advance in flight course
Row processes, and sends instruction to actuator, controls actuator and performs corresponding task, and can need to enter in real time according to actual task
The change of row flight path route and planning.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610414299.4A CN106043693A (en) | 2016-06-14 | 2016-06-14 | Unmanned aerial vehicle for surveying and mapping |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610414299.4A CN106043693A (en) | 2016-06-14 | 2016-06-14 | Unmanned aerial vehicle for surveying and mapping |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106043693A true CN106043693A (en) | 2016-10-26 |
Family
ID=57170880
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610414299.4A Pending CN106043693A (en) | 2016-06-14 | 2016-06-14 | Unmanned aerial vehicle for surveying and mapping |
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| Country | Link |
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| CN (1) | CN106043693A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106598072A (en) * | 2016-12-22 | 2017-04-26 | 徐州飞梦电子科技有限公司 | Unmanned plane operating method for clearing garbage on water surface |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN200939356Y (en) * | 2006-08-22 | 2007-08-29 | 青岛天骄无人机遥感技术有限公司 | Small remote monitoring pilotless plane |
| CN101192064A (en) * | 2006-11-24 | 2008-06-04 | 中国科学院沈阳自动化研究所 | Autonomous flight control system of small unmanned helicopter |
| CN101367436A (en) * | 2008-09-28 | 2009-02-18 | 沈阳锐翼科技有限公司 | Miniature hybrid power flying platform and implementing method thereof |
| CN201334116Y (en) * | 2008-12-01 | 2009-10-28 | 厦门市罗普特科技有限公司 | Hovering police reconnaissance flight vehicle with infra-red range measuring function |
| CN102360218A (en) * | 2011-10-14 | 2012-02-22 | 天津大学 | ARM (advanced RISC (reduced instruction set computer) machines) and FPGA (field-programmable gate array) based navigation and flight control system for unmanned helicopter |
| CN102806990A (en) * | 2012-07-27 | 2012-12-05 | 沈阳航天新光集团有限公司 | Portable mapping unmanned aerial plane |
| CN205168901U (en) * | 2015-11-18 | 2016-04-20 | 山东卫测地理信息科技有限公司 | Automatic height measurement aircraft |
-
2016
- 2016-06-14 CN CN201610414299.4A patent/CN106043693A/en active Pending
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN200939356Y (en) * | 2006-08-22 | 2007-08-29 | 青岛天骄无人机遥感技术有限公司 | Small remote monitoring pilotless plane |
| CN101192064A (en) * | 2006-11-24 | 2008-06-04 | 中国科学院沈阳自动化研究所 | Autonomous flight control system of small unmanned helicopter |
| CN101367436A (en) * | 2008-09-28 | 2009-02-18 | 沈阳锐翼科技有限公司 | Miniature hybrid power flying platform and implementing method thereof |
| CN201334116Y (en) * | 2008-12-01 | 2009-10-28 | 厦门市罗普特科技有限公司 | Hovering police reconnaissance flight vehicle with infra-red range measuring function |
| CN102360218A (en) * | 2011-10-14 | 2012-02-22 | 天津大学 | ARM (advanced RISC (reduced instruction set computer) machines) and FPGA (field-programmable gate array) based navigation and flight control system for unmanned helicopter |
| CN102806990A (en) * | 2012-07-27 | 2012-12-05 | 沈阳航天新光集团有限公司 | Portable mapping unmanned aerial plane |
| CN205168901U (en) * | 2015-11-18 | 2016-04-20 | 山东卫测地理信息科技有限公司 | Automatic height measurement aircraft |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106598072A (en) * | 2016-12-22 | 2017-04-26 | 徐州飞梦电子科技有限公司 | Unmanned plane operating method for clearing garbage on water surface |
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Application publication date: 20161026 |
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