CN106585965A - Unmanned aerial vehicle used for highway surveying - Google Patents
Unmanned aerial vehicle used for highway surveying Download PDFInfo
- Publication number
- CN106585965A CN106585965A CN201610988397.9A CN201610988397A CN106585965A CN 106585965 A CN106585965 A CN 106585965A CN 201610988397 A CN201610988397 A CN 201610988397A CN 106585965 A CN106585965 A CN 106585965A
- Authority
- CN
- China
- Prior art keywords
- unmanned plane
- measuring unit
- inertial measuring
- main frame
- undercarriage
- 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
- 238000005259 measurement Methods 0.000 claims abstract description 4
- 230000002776 aggregation Effects 0.000 claims description 11
- 238000004220 aggregation Methods 0.000 claims description 11
- 230000008054 signal transmission Effects 0.000 claims description 10
- 239000000463 material Substances 0.000 claims description 7
- 229920003023 plastic Polymers 0.000 claims description 6
- 239000004033 plastic Substances 0.000 claims description 6
- 229910000838 Al alloy Inorganic materials 0.000 claims description 4
- 239000000956 alloy Substances 0.000 claims description 4
- 229910001069 Ti alloy Inorganic materials 0.000 claims description 3
- 238000000034 method Methods 0.000 description 4
- 238000010586 diagram Methods 0.000 description 3
- 230000008569 process Effects 0.000 description 3
- 230000003139 buffering effect Effects 0.000 description 2
- 238000013461 design Methods 0.000 description 2
- 239000011257 shell material Substances 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- 230000008859 change Effects 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000008450 motivation Effects 0.000 description 1
- 238000012545 processing Methods 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/08—Helicopters with two or more rotors
-
- 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
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
- G01C11/00—Photogrammetry or videogrammetry, e.g. stereogrammetry; Photographic surveying
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
- G01C21/00—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00
- G01C21/10—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 by using measurements of speed or acceleration
- G01C21/12—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 by using measurements of speed or acceleration executed aboard the object being navigated; Dead reckoning
- G01C21/16—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 by using measurements of speed or acceleration executed aboard the object being navigated; Dead reckoning by integrating acceleration or speed, i.e. inertial navigation
- G01C21/165—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 by using measurements of speed or acceleration executed aboard the object being navigated; Dead reckoning by integrating acceleration or speed, i.e. inertial navigation combined with non-inertial navigation instruments
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
- G01S19/00—Satellite radio beacon positioning systems; Determining position, velocity or attitude using signals transmitted by such systems
- G01S19/38—Determining a navigation solution using signals transmitted by a satellite radio beacon positioning system
- G01S19/39—Determining a navigation solution using signals transmitted by a satellite radio beacon positioning system the satellite radio beacon positioning system transmitting time-stamped messages, e.g. GPS [Global Positioning System], GLONASS [Global Orbiting Navigation Satellite System] or GALILEO
- G01S19/42—Determining position
- G01S19/45—Determining position by combining measurements of signals from the satellite radio beacon positioning system with a supplementary measurement
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
- G01S19/00—Satellite radio beacon positioning systems; Determining position, velocity or attitude using signals transmitted by such systems
- G01S19/38—Determining a navigation solution using signals transmitted by a satellite radio beacon positioning system
- G01S19/39—Determining a navigation solution using signals transmitted by a satellite radio beacon positioning system the satellite radio beacon positioning system transmitting time-stamped messages, e.g. GPS [Global Positioning System], GLONASS [Global Orbiting Navigation Satellite System] or GALILEO
- G01S19/42—Determining position
- G01S19/45—Determining position by combining measurements of signals from the satellite radio beacon positioning system with a supplementary measurement
- G01S19/47—Determining position by combining measurements of signals from the satellite radio beacon positioning system with a supplementary measurement the supplementary measurement being an inertial measurement, e.g. tightly coupled inertial
-
- 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
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/50—On board measures aiming to increase energy efficiency
Landscapes
- Engineering & Computer Science (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Computer Networks & Wireless Communication (AREA)
- Aviation & Aerospace Engineering (AREA)
- Automation & Control Theory (AREA)
- Mechanical Engineering (AREA)
- Multimedia (AREA)
- Position Fixing By Use Of Radio Waves (AREA)
- Navigation (AREA)
Abstract
The invention discloses an unmanned aerial vehicle used for highway surveying. The unmanned aerial vehicle used for highway surveying comprises a laser transmitter, a GPS positioner and a solar panel; a guard circle is connected with a connecting rod; a drive unit is connected with a host through a propeller support; an inertial measuring unit is connected with an undercarriage; a non-skid mat is arranged on the undercarriage; and the right end of the laser transmitter is provided with a high-definition camera. The unmanned aerial vehicle used for highway surveying is innovated on the basis of conventional unmanned aerial vehicles for highway surveying; since the unmanned aerial vehicle provided by the invention is provided with a satellite signal gathering pan, reception of satellite signals becomes more smooth, and measurement errors caused by signal problems are greatly reduced; air springs are arranged on the undercarriage, so the unmanned aerial vehicle is prevented from damage during landing; and the inertial measuring unit and the laser transmitter are arranged and cooperatively used with the GPS positioned, so three-dimensional model information can be measured.
Description
Technical field
The present invention relates to unmanned air vehicle technique field, specially a kind of Highway Survey unmanned plane.
Background technology
Highway Survey unmanned plane is a kind of unmanned plane for geographical information collections such as highway landform, and it is mainly by spiral
This seven portions of oar, solar energy electroplax, guard circle, inertial measuring unit, GPS positioning device, generating laser and high-definition camera
Be grouped into, with science and technology development Highway Survey unmanned plane species it is more and more, for Highway Survey unmanned plane
Demand more and more higher.
And the Highway Survey unmanned plane for currently using also coming with some shortcomings more or less, it is outer than as now used
Shell material matter is mostly the plastics of common process, it is impossible to protect unmanned plane well, and what is had is not provided with satellite-signal aggregation pot, makes
It is not much smoother so as to cause the data for measuring to there is error to obtain satellite signal receiving, and the undercarriage of some settings is not provided with sky
Buffering when gas spring is risen and fallen, it is impossible to protect unmanned plane well so as to which service life substantially reduces, what is had is only provided with
Video camera, is not provided with inertial measuring unit and generating laser, it is impossible to by both in combination with GPS positioning device, it is impossible to very
Good measures three-dimensional model information, it is impossible to the needs that satisfaction is used, so for the presence of such case, it is now desired to carry out phase
The innovative design of pass equipment.
The content of the invention
It is an object of the invention to provide a kind of Highway Survey unmanned plane, to solve above-mentioned background technology in propose show
The plastics of common process are mostly in the enclosure material for using, it is impossible to protect unmanned plane well, what is had is not provided with satellite letter
Number aggregation pot so that satellite signal receiving is not much smoother so as to cause the data for measuring to there is error, and some settings are risen and fallen
Frame is not provided with buffering when air spring is risen and fallen, it is impossible to protect unmanned plane well so as to which service life substantially reduces,
What is had is only provided with video camera, is not provided with inertial measuring unit and generating laser, it is impossible to will both and GPS positioning device phase
With reference to, it is impossible to the problem of three-dimensional model information is measured well.
For achieving the above object, the present invention provides following technical scheme：A kind of Highway Survey unmanned plane, including connection
Bar, guard circle, signal transmission device, high-definition camera, holder, slipmat, undercarriage, connector, driving means, display,
GPS locator, control panel, main frame fixator, fixing nut, solar energy electroplax, battery, screw, propeller bracket, master
Machine, controller, motor and speed changer, also assemble including inertial measuring unit, generating laser, air spring and satellite-signal
Pot, the guard circle is connected with connecting rod, and it is internally provided with driving means, passes through between the driving means and main frame
Propeller bracket is connected, and it is connected with screw, and controller, the controller and electricity are provided with the driving means
Motivation is connected, and speed changer is provided between motor and screw, and the guard circle is connected with solar energy electroplax, described
To electrically connect between battery and controller, it is connected by main frame fixator between the guard circle and main frame, the inertia is surveyed
Signal transmission device is provided with amount device, and its upper end is provided with holder, the inertial measuring unit is connected with undercarriage,
Slipmat is provided with the undercarriage, the right-hand member of the generating laser is provided with high-definition camera, and the satellite-signal gathers
Collection pot is connected with main frame, and the lower end of the GPS locator is provided with display and control panel.
Preferably, the guard circle is provided with two-layer, and per layer is provided with four, each other by solar energy electroplax phase
Connection.
Preferably, the connecting rod be provided with each guard circle eight with, and its material be lightweight engineered plastics.
Preferably, the signal transmission device is provided with two on inertial measuring unit, and both are with regard to inertia measurement dress
Put symmetrical.
Preferably, the undercarriage is provided with four on inertial measuring unit, and is provided with air spring.
Preferably, generally demountable structure that the inertial measuring unit is located, and main frame is located with inertial measuring unit
It is connected by connector between entirety.
Preferably, the motor is provided with two in driving means, and both are symmetrical with regard to controller.
Preferably, the satellite-signal aggregation pot is the concave mirror of an aluminum alloy material, and it is internally provided with GPS and determines
Position device.
Preferably, the upper and lower two-layer of the screw point, per layer is provided with four, and its material is titanium alloy.
Preferably, the battery is provided with four pieces, wherein two pieces is to lead between reserve battery, and solar energy electroplax and battery
Cross fixing nut to be connected.
Compared with prior art, the invention has the beneficial effects as follows：The Highway Survey unmanned plane, with reference to the public affairs for currently using
Exploration unmanned plane in road carries out innovative design, and this Highway Survey unmanned plane employs the industrial light plastics of special process processing
Guard circle and shell are made, the durability of unmanned plane is ensure that well, be provided with satellite-signal aggregation pot so that satellite-signal
Reception becomes more smoothly, greatly reduces and produce measure error due to signal problem, and air is provided with undercarriage
Spring, avoids well when unmanned plane lands and damages unmanned plane, is additionally provided with inertial measuring unit and generating laser, and will
Both can well measure three-dimensional model information in combination with GPS positioning device.
Description of the drawings
Fig. 1 is positive structure diagram of the present invention；
Fig. 2 is overlooking the structure diagram of the present invention；
Fig. 3 is driving device structure schematic diagram of the present invention.
In figure：1st, connecting rod, 2, guard circle, 3, signal transmission device, 4, inertial measuring unit, 5, generating laser, 6, high
Clear video camera, 7, holder, 8, slipmat, 9, air spring, 10, undercarriage, 11, connector, 12, driving means, 13, show
Device, 14, satellite-signal aggregation pot, 15, GPS locator, 16, control panel, 17, main frame fixator, 18, fixing nut, 19, too
It is positive can electroplax, 20, battery, 21, screw, 22, propeller bracket, 23, main frame, 24, controller, 25, motor, 26, speed change
Device.
Specific embodiment
Below in conjunction with the accompanying drawing in the embodiment of the present invention, the technical scheme in the embodiment of the present invention is carried out clear, complete
Site preparation is described, it is clear that described embodiment is only a part of embodiment of the invention, rather than the embodiment of whole.It is based on
Embodiment in the present invention, it is every other that those of ordinary skill in the art are obtained under the premise of creative work is not made
Embodiment, belongs to the scope of protection of the invention.
Fig. 1-3 are referred to, the present invention provides a kind of technical scheme：A kind of Highway Survey unmanned plane, including connecting rod 1,
Guard circle 2, signal transmission device 3, inertial measuring unit 4, generating laser 5, high-definition camera 6, holder 7, slipmat 8, sky
Gas spring 9, undercarriage 10, connector 11, driving means 12, display 13, satellite-signal aggregation pot 14, GPS locator 15, control
Panel processed 16, main frame fixator 17, fixing nut 18, solar energy electroplax 19, battery 20, screw 21, propeller bracket 22, master
Machine 23, controller 24, motor 25 and speed changer 26, guard circle 2 is connected with connecting rod 1, and it is internally provided with driving dress
Put 12, connecting rod 1 is provided with eight with and its material is lightweight engineered plastics, and guard circle 2 is provided with two on each guard circle 2
Layer, and per layer be provided with four, is connected by solar energy electroplax 19 each other, battery 20 is provided with four pieces, wherein two pieces
To be connected by fixing nut 18 between reserve battery 20, and solar energy electroplax 19 and battery 20, driving means 12 and main frame
It is connected by propeller bracket 22 between 23, and it is connected with screw 21, two-layer about 21 points of screw, per layer of setting
There are four, and its material is to be provided with controller 24 in titanium alloy, driving means 12, controller 24 is connected with motor 25,
And speed changer 26 is provided between motor 25 and screw 21, motor 25 is provided with two, and two in driving means 12
Person is symmetrical with regard to controller 24, and guard circle 2 is connected with solar energy electroplax 19, to electrically connect between battery 20 and controller 24,
It is connected by main frame fixator 17 between guard circle 2 and main frame 23, signal transmission device 3 is provided with inertial measuring unit 4, and
Its upper end is provided with holder 7, and signal transmission device 3 is provided with two on inertial measuring unit 4, and both are with regard to inertia measurement
Device 4 is symmetrical, and inertial measuring unit 4 is connected with undercarriage 10, generally demountable structure that inertial measuring unit 4 is located, and
Main frame 23 is located between entirety with inertial measuring unit 4 and is connected by connector 11, and undercarriage 10 is on inertial measuring unit 4
Four are provided with, and are provided with air spring 9, can be good at providing cushioning effect, undercarriage for the landing of unmanned plane
Slipmat 8 is provided with 10, the right-hand member of generating laser 5 is provided with high-definition camera 6, and satellite-signal aggregation pot is connected with main frame
Connect, satellite-signal aggregation pot 14 is the concave mirror of an aluminum alloy material, and it is internally provided with GPS locator 15, GPS location
The lower end of device 15 is provided with display 13 and control panel 16.
Operation principle：Before using the Highway Survey unmanned plane, needs are carried out to whole Highway Survey with unmanned plane
Simple structure understands, first check before the use battery 20, screw 21 and holder 7 whether can normal work, then
Path coordinate control point is travelled by the input of control panel 16 and related auxiliary parameter, and startup power supply are set, then by letter
Number transmitter 3 carries out the transmission of data and instruction with remote control, and then unmanned plane just flies according to the control point path for arranging,
Inertial measuring unit 4, generating laser 5 and high-definition camera 6 can enter line number in combination with GPS locator 15 in flight course
The three-dimensional coordinate information of word elevation model and the shooting of image, satellite-signal aggregation pot 14 is the back taper of an aluminum alloy material
Shape, and it is internally provided with GPS locator 15, satellite-signal can be gathered position of feeling terribly worried by satellite-signal aggregation pot 14
In GPS locator 15, the unimpeded of signal is ensure that well, here it is the workflow of whole Highway Survey unmanned plane.
Although being described in detail to the present invention with reference to the foregoing embodiments, for a person skilled in the art,
It still can modify to the technical scheme described in foregoing embodiments, or which part technical characteristic is carried out etc.
With replacing, all any modification, equivalent substitution and improvements within the spirit and principles in the present invention, made etc. should be included in this
Within the protection domain of invention.
Claims (10)
1. a kind of Highway Survey unmanned plane, including connecting rod（1）, guard circle（2）, signal transmission device（3）, high-definition camera
（6）, holder（7）, slipmat（8）, undercarriage（10）, connector（11）, driving means（12）, display（13）, GPS location
Device（15）, control panel（16）, main frame fixator（17）, fixing nut（18）, solar energy electroplax（19）, battery（20）, spiral
Oar（21）, propeller bracket（22）, main frame（23）, controller（24）, motor（25）And speed changer（26）, it is characterised in that：
Also include inertial measuring unit（4）, generating laser（5）, air spring（9）Assemble pot with satellite-signal（14）, the protection
Circle（2）With connecting rod（1）It is connected, and it is internally provided with driving means（12）, the driving means（12）With main frame（23）
Between pass through propeller bracket（22）It is connected, and itself and screw（21）It is connected, the driving means（12）Inside it is provided with
Controller（24）, the controller（24）With motor（25）It is connected, and motor（25）With screw（21）Between arrange
There is speed changer（26）, the guard circle（2）With solar energy electroplax（19）It is connected, the battery（20）With controller（24）Between
For electrical connection, the guard circle（2）With main frame（23）Between pass through main frame fixator（17）It is connected, the inertial measuring unit
（4）On be provided with signal transmission device（3）, and its upper end is provided with holder（7）, the inertial measuring unit（4）With undercarriage
（10）It is connected, the undercarriage（10）On be provided with slipmat（8）, the generating laser（5）Right-hand member be provided with high definition
Video camera（6）, the satellite-signal aggregation pot（14）With main frame（23）It is connected, the GPS locator（15）Lower end arrange
There is display（13）And control panel（16）.
2. a kind of Highway Survey unmanned plane according to claim 1, it is characterised in that：The guard circle（2）It is provided with
Two-layer, and per layer be provided with four, each other by solar energy electroplax（19）It is connected.
3. a kind of Highway Survey unmanned plane according to claim 1, it is characterised in that：The connecting rod（1）At each
Guard circle（2）On be provided with eight, and its material is lightweight engineered plastics.
4. a kind of Highway Survey unmanned plane according to claim 1, it is characterised in that：The signal transmission device（3）
Inertial measuring unit（4）On be provided with two, and both are with regard to inertial measuring unit（4）Symmetrically.
5. a kind of Highway Survey unmanned plane according to claim 1, it is characterised in that：The undercarriage（10）In inertia
Measurement apparatus（4）On be provided with four, and be provided with air spring（9）.
6. a kind of Highway Survey unmanned plane according to claim 1, it is characterised in that：The inertial measuring unit（4）
Be located generally demountable structure, and main frame（23）With inertial measuring unit（4）Pass through connector between the entirety of place（11）Phase
Connection.
7. a kind of Highway Survey unmanned plane according to claim 1, it is characterised in that：The motor（25）Driving
Device（12）Two are inside provided with, and both are with regard to controller（24）Symmetrically.
8. a kind of Highway Survey unmanned plane according to claim 1, it is characterised in that：The satellite-signal assembles pot
（14）For the concave mirror of an aluminum alloy material, and it is internally provided with GPS locator（15）.
9. a kind of Highway Survey unmanned plane according to claim 1, it is characterised in that：The screw（21）Divide upper and lower
Two-layer, per layer is provided with four, and its material is titanium alloy.
10. a kind of Highway Survey unmanned plane according to claim 1, it is characterised in that：The battery（20）It is provided with
Four pieces, wherein two pieces is reserve battery（20）, and solar energy electroplax（19）With battery（20）Between pass through fixing nut（18）Phase
Connection.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610988397.9A CN106585965A (en) | 2016-12-30 | 2016-12-30 | Unmanned aerial vehicle used for highway surveying |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610988397.9A CN106585965A (en) | 2016-12-30 | 2016-12-30 | Unmanned aerial vehicle used for highway surveying |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106585965A true CN106585965A (en) | 2017-04-26 |
Family
ID=58590949
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610988397.9A Pending CN106585965A (en) | 2016-12-30 | 2016-12-30 | Unmanned aerial vehicle used for highway surveying |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106585965A (en) |
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107323659A (en) * | 2017-06-22 | 2017-11-07 | 深圳市雷凌广通技术研发有限公司 | A kind of Intelligent unattended machine for being easy to store based on Internet of Things |
| CN107544537A (en) * | 2017-08-30 | 2018-01-05 | 中北大学 | A kind of anti-tampering power-line patrolling unmanned plane |
| CN108082456A (en) * | 2018-01-23 | 2018-05-29 | 张烨园 | A kind of mounting structure of unmanned plane fixed frame |
| CN108791831A (en) * | 2018-06-17 | 2018-11-13 | 赖海燕 | A kind of agricultural unmanned plane landing anti-collision protection device |
| CN109131860A (en) * | 2018-09-18 | 2019-01-04 | 华北水利水电大学 | The plant protection drone of view-based access control model |
| CN111776214A (en) * | 2020-06-17 | 2020-10-16 | 广东工业大学 | Real-time imaging device for road survey |
| CN112874753A (en) * | 2021-02-18 | 2021-06-01 | 陶霖密 | Integrated platy laminated rack unmanned aerial vehicle |
| CN114894163A (en) * | 2022-05-24 | 2022-08-12 | 中国地质科学院岩溶地质研究所 | Geological disaster hidden danger detection method for multi-unmanned aerial vehicle collaborative photogrammetry |
Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN202600150U (en) * | 2012-05-17 | 2012-12-12 | 北京必威易激光科技有限公司 | Intelligent low-altitude remote sensing surveying and mapping system |
| CN204575069U (en) * | 2015-04-14 | 2015-08-19 | 武汉海达数云技术有限公司 | The airborne three-dimensional laser measurement mechanism of a kind of SUAV (small unmanned aerial vehicle) |
| CN206307269U (en) * | 2016-12-30 | 2017-07-07 | 苏州曾智沃德智能科技有限公司 | A kind of Highway Survey unmanned plane |
-
2016
- 2016-12-30 CN CN201610988397.9A patent/CN106585965A/en active Pending
Patent Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN202600150U (en) * | 2012-05-17 | 2012-12-12 | 北京必威易激光科技有限公司 | Intelligent low-altitude remote sensing surveying and mapping system |
| CN204575069U (en) * | 2015-04-14 | 2015-08-19 | 武汉海达数云技术有限公司 | The airborne three-dimensional laser measurement mechanism of a kind of SUAV (small unmanned aerial vehicle) |
| CN206307269U (en) * | 2016-12-30 | 2017-07-07 | 苏州曾智沃德智能科技有限公司 | A kind of Highway Survey unmanned plane |
Cited By (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107323659A (en) * | 2017-06-22 | 2017-11-07 | 深圳市雷凌广通技术研发有限公司 | A kind of Intelligent unattended machine for being easy to store based on Internet of Things |
| CN107544537A (en) * | 2017-08-30 | 2018-01-05 | 中北大学 | A kind of anti-tampering power-line patrolling unmanned plane |
| CN107544537B (en) * | 2017-08-30 | 2020-05-22 | 中北大学 | Anti-interference electric power line patrol unmanned aerial vehicle |
| CN108082456A (en) * | 2018-01-23 | 2018-05-29 | 张烨园 | A kind of mounting structure of unmanned plane fixed frame |
| CN108791831A (en) * | 2018-06-17 | 2018-11-13 | 赖海燕 | A kind of agricultural unmanned plane landing anti-collision protection device |
| CN109131860A (en) * | 2018-09-18 | 2019-01-04 | 华北水利水电大学 | The plant protection drone of view-based access control model |
| CN109131860B (en) * | 2018-09-18 | 2024-01-23 | 华北水利水电大学 | Plant protection unmanned aerial vehicle based on vision |
| CN111776214A (en) * | 2020-06-17 | 2020-10-16 | 广东工业大学 | Real-time imaging device for road survey |
| CN112874753A (en) * | 2021-02-18 | 2021-06-01 | 陶霖密 | Integrated platy laminated rack unmanned aerial vehicle |
| CN114894163A (en) * | 2022-05-24 | 2022-08-12 | 中国地质科学院岩溶地质研究所 | Geological disaster hidden danger detection method for multi-unmanned aerial vehicle collaborative photogrammetry |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN106585965A (en) | Unmanned aerial vehicle used for highway surveying | |
| CN104386249B (en) | The mapping method of the many rotor wing unmanned aerial vehicles of a kind of quick mapping | |
| CN101887037B (en) | Wheel-type X-ray flaw detection robot device | |
| CN103963963B (en) | The flight control method of multi-rotor aerocraft and system | |
| CN204236777U (en) | The many rotor wing unmanned aerial vehicles of a kind of mapping fast | |
| CN104535048B (en) | A kind of unmanned vehicle remote sensing system and unmanned vehicle remote sensing technique | |
| CN212332992U (en) | Multifunctional three-light nacelle and system based on unmanned aerial vehicle carrying and unmanned aerial vehicle | |
| CN106813900B (en) | A kind of civil airport navigational lighting aid flight check method based on unmanned air vehicle technique | |
| CN105644752A (en) | Novel wind-solar complementary power supply type unmanned sailing ship and control method thereof | |
| CN206704529U (en) | A kind of camera oblique photograph unmanned plane of four rotor five | |
| CN108400554A (en) | Utilize the method for unmanned plane inspection overhead transmission line | |
| JP6811976B2 (en) | Aircraft | |
| CN206307269U (en) | A kind of Highway Survey unmanned plane | |
| CN103792957A (en) | Light two-freedom-degree camera stabilized platform device | |
| CN113148156A (en) | Many rotor unmanned aerial vehicle with barrier function is kept away to laser intelligence | |
| CN113900453B (en) | Precise docking control method and system for aerial charging mother-son unit of quad-rotor unmanned aerial vehicle | |
| CN204473159U (en) | A kind of mount pad of rotating camera of holder for aerial photographing | |
| CN208506246U (en) | A kind of device suitable for the positioning of chimney inside processing flying platform | |
| CN105136484A (en) | Inter-shaft four-wheel positioning detection device and detection method | |
| CN209842051U (en) | Installation mechanism of laser radar on unmanned aerial vehicle | |
| CN116513524A (en) | Urban planning mapping equipment based on unmanned aerial vehicle remote sensing mapping | |
| CN207851280U (en) | A kind of laser radar apparatus | |
| CN113074698B (en) | Intelligent tower inclination detection system based on machine vision | |
| CN110217400A (en) | A kind of patrol unmanned machine of interior anticollision industry | |
| CN110065642A (en) | A kind of urban viaduct detection unmanned plane |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20170426 |
|
| WD01 | Invention patent application deemed withdrawn after publication |