CN108357690A - A kind of movable unmanned helicopter airplane parking area of laser aiming - Google Patents
A kind of movable unmanned helicopter airplane parking area of laser aiming Download PDFInfo
- Publication number
- CN108357690A CN108357690A CN201810227063.9A CN201810227063A CN108357690A CN 108357690 A CN108357690 A CN 108357690A CN 201810227063 A CN201810227063 A CN 201810227063A CN 108357690 A CN108357690 A CN 108357690A
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- Prior art keywords
- parking area
- airplane parking
- laser
- berth
- unmanned helicopter
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- 238000006243 chemical reaction Methods 0.000 claims description 6
- 238000004891 communication Methods 0.000 claims description 6
- 230000000903 blocking effect Effects 0.000 description 2
- 230000006835 compression Effects 0.000 description 2
- 238000007906 compression Methods 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 239000007788 liquid Substances 0.000 description 2
- 238000005259 measurement Methods 0.000 description 2
- 238000002156 mixing Methods 0.000 description 2
- 230000000007 visual effect Effects 0.000 description 2
- 235000008429 bread Nutrition 0.000 description 1
- 238000013461 design Methods 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 239000011229 interlayer Substances 0.000 description 1
- 239000003550 marker Substances 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000010248 power generation Methods 0.000 description 1
- 238000012546 transfer Methods 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F1/00—Ground or aircraft-carrier-deck installations
- B64F1/007—Helicopter portable landing pads
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F1/00—Ground or aircraft-carrier-deck installations
- B64F1/18—Visual or acoustic landing aids
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F1/00—Ground or aircraft-carrier-deck installations
- B64F1/18—Visual or acoustic landing aids
- B64F1/20—Arrangement of optical beacons
Abstract
A kind of movable unmanned helicopter airplane parking area of laser aiming, idler wheel is installed in the shaft of the application movement airplane parking area main body both sides, respectively there are one hydraulic stems at four angles of mobile airplane parking area main body, lift the upper end that berth is mounted on the telescopic rod of hydraulic stem, there is the H-type mark of landing point in the middle part of lifting berth, the middle part of H-type mark is Laser emission mouth, lifting berth both sides, respectively there are one solar panels, respectively there are a pair of of horizontal rotation motor in the both sides in lifting berth, the horizontal rotation machine shaft for rotating horizontally motor is connected by connecting rod, there is vertical electric rotating machine in the side of solar panel, vertical electric rotating machine shaft is connected with bar middle part is correspondingly connected with.The usable laser of the application carries out the movable unmanned helicopter airplane parking area of landing guiding; using laser beam high directivity, wave beam is narrow, anti-interference ability powerful feature, also, airplane parking area itself is removable; landing plane can automatic leveling, to substantially increase the adaptability under complex environment.
Description
Technical field
The present invention relates to unmanned plane stopping pad fields, are shut down more particularly to a kind of movable unmanned helicopter of laser aiming
Level ground.
Background technology
With the continuous development of unmanned air vehicle technique, unmanned plane has higher requirement in landing to visual environment, manually
Landing needs winged hand to confirm the environment of drop point with avoiding obstacles using onboard image equipment and select relatively flat earth's surface, but
At night or in visual poor environment（Such as haze）The security risk landed manually is larger, it is therefore desirable to which design makes accordingly
With the movable unmanned helicopter airplane parking area of laser aiming.
Invention content
Above-mentioned in order to solve the problems, such as, the present invention provides a kind of movable unmanned helicopter airplane parking area of laser aiming, can
The movable unmanned helicopter airplane parking area that landing guiding is carried out using laser, using laser beam high directivity, wave beam is narrow, anti-interference energy
Power powerful feature, also, airplane parking area itself is removable, landing plane can automatic leveling, to substantially increase under complex environment
Adaptability, for this purpose, the present invention provides a kind of movable unmanned helicopter airplane parking area of laser aiming, including mobile airplane parking area
Main body, idler wheel, hydraulic stem, solar panel and lifting berth, are equipped in the shaft of the mobile airplane parking area main body both sides
Idler wheel, respectively there are one hydraulic stem, the lifting berth is mounted on the flexible of hydraulic stem at four angles of the mobile airplane parking area main body
The upper end of bar, the lifting berth internal control coremaking piece have Attitude Measuring Unit, there is the H-type mark of landing point in the middle part of the lifting berth
The middle part of will, the H-type mark is Laser emission mouth, and laser emitter, the lifting pool are provided in the Laser emission mouth
Respectively there are one solar panel, the both sides in the lifting berth respectively have a pair to rotate horizontally motor, the horizontal rotation for position both sides
The horizontal rotation machine shaft of rotating motor is connected by connecting rod, there is vertical rotation electric rotating in the side of the solar panel
Machine, the vertical electric rotating machine shaft are connected with bar middle part is correspondingly connected with.
Further improvement of the present invention, respectively there are one LED light at four angles in the lifting berth, and LED light can be at night
It reacts the position of airplane parking area and carries out drop point determination.
Respectively there are the locking mechanism and fastener of retaining mechanism in further improvement of the present invention, the mobile airplane parking area main body both sides
The locking mechanism of structure, the retaining mechanism is traction lock padlock locking structure, and the fastener structures of the retaining mechanism are traction lock
Fastener structures are detained, the present invention can be with the multiple connected uses of blocking.
Further improvement of the present invention, the laser emitter laser wavelength are the laser of 10.6 micron wavebands, and 10.6 is micro-
The laser of VHF band can use under conditions of poor visibility.
Further improvement of the present invention, the Attitude Measuring Unit are a rectangular circuit board, the rectangular circuit board front
It is connect including GPS antenna, power conversion chip, three-axis gyroscope, magnetic sensor, three axis accelerometer, USB interface and contact pin
Mouthful, the GPS antenna bottom is GPS antenna feed point, and the rectangular circuit board reverse side includes GPS chip, microcontroller and communication
Chip, and fixed by four fixed hole positions, there are two rows of spare interfaces, GPS chip and GPS antenna in the rectangular circuit board side
For the time service and positioning of system, power conversion chip generates the voltage needed for Attitude Measuring Unit work, usb communication chip and
USB interface is used for the output of posture and location information, and posture blending algorithm uses three-axis gyroscope, magnetic sensor and three axis
The output of accelerometer calculates the real-time attitude of platform.Contact pin interface is the expansion interface reserved.
The present invention provides a kind of movable unmanned helicopter airplane parking area of laser aiming, car body, traction lock, berth, four liquid
Compression bar, two blocks of solar-powered collapsible plates, the rotary shaft for connecting solar panel, berth, laser emitter, four position instructions
Lamp and built-in Attitude Measuring Unit module composition, using laser beam high directivity, wave beam is narrow, strong antijamming capability, especially
The laser of 10.6 micron wavebands can use under conditions of poor visibility, then coordinate airplane parking area itself removable and landing is flat
Face can automatic leveling, solar panel can by vertical electric rotating machine carry out rotary turning, so only need to be arranged on one side too
Positive energy solar panel just can be carried out solar power generation in expansion and closure situation, substantially increase airplane parking area under complex environment
Adaptability.
Description of the drawings
Fig. 1 is schematic structural view of the invention one；
Fig. 2 is schematic structural view of the invention two；
Fig. 3 is Attitude Measuring Unit chip schematic diagram one of the present invention；
Fig. 4 is Attitude Measuring Unit chip schematic diagram two of the present invention；
It illustrates:
1, mobile airplane parking area main body；2, idler wheel；3, traction lock padlock locking structure；4, traction lock fastener structures；5, hydraulic stem；6,
Solar panel；7, vertical electric rotating machine shaft；8, rotate horizontally machine shaft；9, lift berth；10, Laser emission mouth；
11, rectangular circuit board；12, fixed hole position；13, communication chip；14, microcontroller；15, GPS antenna feed point；16, three axis accelerometer
Instrument；17, magnetic sensor；18, GPS antenna；19, USB interface；20, power conversion chip；21, spare interface；22, three axis
Accelerometer.
Specific implementation mode
Present invention is further described in detail with specific implementation mode below in conjunction with the accompanying drawings：
The present invention provides a kind of movable unmanned helicopter airplane parking area of laser aiming, and usable laser carries out the movable type of landing guiding
Unmanned plane airplane parking area, using laser beam high directivity, wave beam is narrow, anti-interference ability powerful feature, also, airplane parking area itself is removable
It is dynamic, landing plane can automatic leveling, to substantially increase the adaptability under complex environment.
As an embodiment of the present invention, the present invention provides a kind of movable unmanned helicopter airplane parking area of laser aiming, including
Mobile airplane parking area main body 1, idler wheel 2, hydraulic stem 5, solar panel 6 and lifting berth 9,1 liang of the mobile airplane parking area main body
Idler wheel 2 is installed, respectively there are one hydraulic stem 5, the lifting berths at four angles of the mobile airplane parking area main body 1 in the shaft of side
9 are mounted on the upper end of the telescopic rod of hydraulic stem 5, and there are the H-type mark of landing point, the lifting berth 9 in 9 middle part of lifting berth
Internal control coremaking piece has Attitude Measuring Unit, and the middle part of the H-type mark is Laser emission mouth 10, is set in the Laser emission mouth 10
It is equipped with laser emitter, respectively there are one solar panel 6, the both sides in the lifting berth 9 respectively have for 9 both sides of lifting berth
A pair rotates horizontally motor, and the horizontal rotation machine shaft 8 for rotating horizontally motor is connected by connecting rod, the solar energy
There are vertical rotation electric rotating machine, the vertical electric rotating machine shaft 7 to be connected with bar middle part is correspondingly connected in the side of solar panel 6.
As a kind of specific embodiment of the present invention, the present invention provides a kind of movable type of laser aiming as shown in Figs. 1-2
Unmanned plane airplane parking area, including mobile airplane parking area main body 1, idler wheel 2, hydraulic stem 5, solar panel 6 and lifting berth 9, it is described
Idler wheel 2 is installed, respectively there are one liquid at four angles of the mobile airplane parking area main body 1 in the shaft of 1 both sides of mobile airplane parking area main body
Compression bar 5, it is described lifting berth 9 be mounted on hydraulic stem 5 telescopic rod upper end, it is described lifting berth 9 four angles it is each there are one
LED light, LED light can react the position of airplane parking area at night and carry out drop point determination, and there is landing point at 9 middle part of the lifting berth
H-type mark, 9 internal control coremaking piece of the lifting berth has an Attitude Measuring Unit, and the middle part of the H-type mark is Laser emission mouth
10, laser emitter is provided in the Laser emission mouth 10, the laser emitter laser wavelength is 10.6 micron wavebands
The laser of laser, 10.6 micron wavebands can use under conditions of poor visibility, and respectively there are one too for 9 both sides of lifting berth
Respectively there are a pair of of horizontal rotation motor, the level rotation for rotating horizontally motor in the both sides of positive energy solar panel 6, the lifting berth 9
Rotating motor shaft 8 is connected by connecting rod, there is vertical electric rotating machine, the vertical rotation in the side of the solar panel 6
Rotating motor shaft 7 is connected with bar middle part is correspondingly connected with, and respectively there are the locking mechanism of retaining mechanism in the mobile airplane parking area main body both sides
And fastener structures, the locking mechanism of the retaining mechanism is traction lock padlock locking structure 3, and the fastener structures of the retaining mechanism are
Traction lock fastener structures 4, the present invention can be with the multiple connected uses of blocking.
Attitude Measuring Unit of the present invention is a rectangular circuit board, the positive bread of rectangular circuit board as shown in Figures 3 and 4
GPS antenna, power conversion chip, three-axis gyroscope, magnetic sensor, three axis accelerometer, USB interface and contact pin is included to connect
Mouthful, the GPS antenna bottom is GPS antenna feed point, and the rectangular circuit board reverse side includes GPS chip, microcontroller and communication
Chip, and fixed by four fixed hole positions, there are two rows of spare interfaces, GPS chip and GPS antenna in the rectangular circuit board side
For the time service and positioning of system, power conversion chip generates the voltage needed for Attitude Measuring Unit work, usb communication chip and
USB interface is used for the output of posture and location information, and posture blending algorithm uses three-axis gyroscope, magnetic sensor and three axis
The output of accelerometer calculates the real-time attitude of platform.Contact pin interface is the expansion interface reserved.
Characteristics of components of the present invention：Berth center depicts the H-type mark for indicating landing point, the circle in circle marker region
Interior portion has disposed a laser emitter, and the direction of the launch is vertical with berth upper surface and points into the sky, and the length of transmitter is not
More than berth thickness so that it can be embedded in the interlayer of berth without causing surface bulge.Four ends of berth upper surface
Point is respectively there are one high-brightness LED, the boundary for indicating airplane parking area.Four endpoints of berth lower surface respectively connect there are one hydraulic stem
For adjusting height, the lifting in berth may be implemented and the horizontal reference in berth is adjusted, to ensure aircraft landing
Shi Bowei is parallel with local level.The lower surface in berth is equipped with attitude measurement module, is used to measure berth in real time
Posture, if find and the angled deviation of local level, control hydraulic stem and be adjusted.Berth both sides are respectively provided with the sun
Energy plate provides electric energy for whole system, and two pieces of solar panels are attached by specific two degrees of freedom rotary shaft respectively, in water
Solar panels may be implemented opening and closing movement under the drive of flat axis, and plate is opened when work, and solar panels merge to reduce when not working
Volume；The rotation along axial direction may be implemented in solar panels under the drive of vertical axes, by being improved too to the tracking of light source
The transfer efficiency of positive energy plate.Car body front end is equipped with the protruding end of traction lock, and body rear end is equipped with the lock ring of traction lock,
Front and back car body can be attached by this traction locker and be formed a team, and be disposed by headstock traction traveling to designated position.
When normal work, airplane parking area is drawn to designated position by headstock first, deploying solar plate simultaneously enters working condition,
Berth pushes to height appropriate by hydraulic stem, and the level in berth is kept under the auxiliary of attitude measurement module.When there is nobody
When machine approaching touch down, by the laser seeker or infrared thermoviewer of aircraft bottom（Since the energy of laser beam is stronger, at
As the very high white point of brightness can be formed on instrument, so being easy for that it can be positioned）Receive what airplane parking area emitted
Laser can also be according to the LED lamplight of airplane parking area quadrangle to drop point site in descent to complete from motion tracking and land
It is further confirmed that.
The above described is only a preferred embodiment of the present invention, being not the limit for making any other form to the present invention
System, and according to the technical essence of the invention made by any modification or equivalent variations, still fall within present invention model claimed
It encloses.
Claims (7)
1. a kind of movable unmanned helicopter airplane parking area of laser aiming, including mobile airplane parking area main body（1）, idler wheel（2）, hydraulic stem
（5）, solar panel（6）With lifting berth（9）, it is characterised in that：The mobile airplane parking area main body（1）In the shaft of both sides
Idler wheel is installed（2）, the mobile airplane parking area main body（1）Four angles respectively there are one hydraulic stem（5）, the lifting berth（9）
Mounted on hydraulic stem（5）Telescopic rod upper end, the lifting berth（9）Internal control coremaking piece has Attitude Measuring Unit, the liter
Berth drops（9）There is the H-type mark of landing point at middle part, and the middle part of the H-type mark is Laser emission mouth（10）, the Laser emission
Mouthful（10）Inside it is provided with laser emitter, the lifting berth（9）Respectively there are one solar panels for both sides（6）, the lifting
Berth（9）Both sides respectively have and a pair of rotate horizontally motor, the horizontal rotation machine shaft for rotating horizontally motor（8）Pass through company
Extension bar is connected, the solar panel（6）Side in have vertical electric rotating machine, the vertical electric rotating machine shaft（7）With
It is correspondingly connected in the middle part of bar and is connected.
2. a kind of movable unmanned helicopter airplane parking area of laser aiming according to claim 1, it is characterised in that：The lifting
Berth（9）Four angles respectively there are one LED light.
3. a kind of movable unmanned helicopter airplane parking area of laser aiming according to claim 1, it is characterised in that：The movement
Airplane parking area main body（1）Respectively there are the locking mechanism and fastener structures of retaining mechanism in both sides.
4. a kind of movable unmanned helicopter airplane parking area of laser aiming according to claim 3, it is characterised in that：The locking
The locking mechanism of mechanism is traction lock padlock locking structure（3）, the fastener structures of the retaining mechanism are traction lock fastener structures.
5. a kind of movable unmanned helicopter airplane parking area of laser aiming according to claim 1, it is characterised in that：The laser
Transmitter laser wavelength is the laser of 10.6 micron wavebands.
6. a kind of movable unmanned helicopter airplane parking area of laser aiming according to claim 1, it is characterised in that：The posture
Measuring unit is a rectangular circuit board（11）, the rectangular circuit board（11）Front includes GPS antenna（18）, power conversion chip
（20）, three-axis gyroscope（16）, magnetic sensor（17）, three axis accelerometer（22）, USB interface（19）And contact pin interface,
The GPS antenna（18）Bottom is GPS antenna feed point（15）, the rectangular circuit board（11）Reverse side includes GPS chip（13）, it is micro-
Controller（14）And communication chip（13）, and pass through four fixed hole positions（12）It is fixed.
7. a kind of movable unmanned helicopter airplane parking area of laser aiming according to claim 6, it is characterised in that：The rectangle
Circuit board（11）There are two rows of spare interfaces in side（21）.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810227063.9A CN108357690A (en) | 2018-03-20 | 2018-03-20 | A kind of movable unmanned helicopter airplane parking area of laser aiming |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810227063.9A CN108357690A (en) | 2018-03-20 | 2018-03-20 | A kind of movable unmanned helicopter airplane parking area of laser aiming |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN108357690A true CN108357690A (en) | 2018-08-03 |
Family
ID=63000990
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810227063.9A Pending CN108357690A (en) | 2018-03-20 | 2018-03-20 | A kind of movable unmanned helicopter airplane parking area of laser aiming |
Country Status (1)
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| CN (1) | CN108357690A (en) |
Cited By (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109778725A (en) * | 2019-03-18 | 2019-05-21 | 深圳基原中正工程建设有限公司 | Auto-folder handling can transport formula airplane parking area |
| CN109866936A (en) * | 2019-03-14 | 2019-06-11 | 燕山大学 | UAV Landing based on six degree of freedom hybrid mechanism recycles integrated mobile platform |
| CN110096065A (en) * | 2019-04-09 | 2019-08-06 | 惠州市三航无人机技术研究院 | A kind of quadrotor drone attitude-control device |
| CN110104194A (en) * | 2019-04-28 | 2019-08-09 | 河北工业大学 | A kind of hatch door eversion type small drone is berthed cabin |
| CN110293858A (en) * | 2019-06-24 | 2019-10-01 | 大连理工大学 | A kind of continuous self monitor method and device based on unmanned plane and intelligent airplane parking area |
| CN110908403A (en) * | 2019-12-09 | 2020-03-24 | 国家电网有限公司 | Automatic fixed-point landing device and method for electric power line patrol unmanned aerial vehicle |
| CN112441248A (en) * | 2020-11-23 | 2021-03-05 | 广东电科院能源技术有限责任公司 | Unmanned aerial vehicle-mounted airport and control method thereof |
| WO2021055402A1 (en) * | 2018-04-27 | 2021-03-25 | Newcomb Royce | Portable landing and take-off pad for an unmanned air aerial vehicle |
| CN113844557A (en) * | 2021-10-26 | 2021-12-28 | 广东电网有限责任公司 | Unmanned aerial vehicle shuts down nest and unmanned aerial vehicle electric power fortune dimension system |
| CN114435614A (en) * | 2020-11-05 | 2022-05-06 | 北星空间信息技术研究院(南京)有限公司 | Method for dynamically landing ground robot by unmanned aerial vehicle |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2021055402A1 (en) * | 2018-04-27 | 2021-03-25 | Newcomb Royce | Portable landing and take-off pad for an unmanned air aerial vehicle |
| CN109866936A (en) * | 2019-03-14 | 2019-06-11 | 燕山大学 | UAV Landing based on six degree of freedom hybrid mechanism recycles integrated mobile platform |
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| CN110908403A (en) * | 2019-12-09 | 2020-03-24 | 国家电网有限公司 | Automatic fixed-point landing device and method for electric power line patrol unmanned aerial vehicle |
| CN114435614A (en) * | 2020-11-05 | 2022-05-06 | 北星空间信息技术研究院(南京)有限公司 | Method for dynamically landing ground robot by unmanned aerial vehicle |
| CN112441248A (en) * | 2020-11-23 | 2021-03-05 | 广东电科院能源技术有限责任公司 | Unmanned aerial vehicle-mounted airport and control method thereof |
| CN112441248B (en) * | 2020-11-23 | 2022-07-19 | 南方电网电力科技股份有限公司 | Vehicle-mounted airport of unmanned aerial vehicle and control method thereof |
| CN113844557A (en) * | 2021-10-26 | 2021-12-28 | 广东电网有限责任公司 | Unmanned aerial vehicle shuts down nest and unmanned aerial vehicle electric power fortune dimension system |
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Application publication date: 20180803 |