CN106742016A - A kind of SUAV reclaims understructure - Google Patents
A kind of SUAV reclaims understructure Download PDFInfo
- Publication number
- CN106742016A CN106742016A CN201710004602.8A CN201710004602A CN106742016A CN 106742016 A CN106742016 A CN 106742016A CN 201710004602 A CN201710004602 A CN 201710004602A CN 106742016 A CN106742016 A CN 106742016A
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- CN
- China
- Prior art keywords
- unmanned plane
- landing stage
- processor
- micromatic setting
- position sensor
- 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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Classifications
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- 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
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
Abstract
Understructure, including Landing stage and slide rail are reclaimed the invention discloses a kind of SUAV, the Landing stage bottom is provided with micromatic setting, and Landing stage is connected by micromatic setting with slide assemblies, and slide assemblies are matched with slide rail.After unmanned plane is dropped on Landing stage, Landing stage is moved along slide rail, and unmanned plane directly is sent into hangar；Position sensor and processor are additionally provided with the Landing stage, processor is connected with position sensor, micromatic setting and slide assemblies respectively.It is an advantage of the invention that：Landing stage can be acted with the motion of unmanned plane, make the Landing stage center that unmanned plane lands；Directly hangar can be sent into after unmanned plane landing along slide rail.
Description
Technical field
Instrument is reclaimed the present invention relates to a kind of unmanned plane, and in particular to a kind of SUAV reclaims understructure.
Background technology
Referred to as " unmanned plane ", english abbreviation is " UAV " to UAV, using radio robot and providing for oneself
The not manned aircraft that presetting apparatus is manipulated.Can be divided into from technical standpoint definition：Unmanned fixed-wing aircraft, unmanned VTOL
Machine, unmanned airship, depopulated helicopter, unmanned multi-rotor aerocraft, unmanned parasol etc..Unmanned plane presses application field, can be divided into
It is military with it is civilian.Military aspect, unmanned plane is divided into reconnaissance plane and target drone.Civilian aspect, unmanned plane+sector application is unmanned plane
Real firm need；At present taking photo by plane, agricultural, plant protection, auto heterodyne, express transportation, disaster relief, observation wild animal, monitoring infection
The application in disease, mapping, news report, electric inspection process, the disaster relief, movies-making, manufacture romance etc. field, has greatly expanded nothing
The man-machine purposes of itself, developed country is also in actively extension sector application and development unmanned air vehicle technique.In November, 2013, middle its people
With aviation, office issues《Civilian push-button aircraft system driver management temporary provisions》, the people are responsible for by Chinese AOPA associations
With the related management of unmanned plane.According to《Regulation》, inland of China unmanned plane is operated can be divided into 11 according to type size, flying area
The situation of kind, wherein only more than 116 kilograms of unmanned plane and more than 4600 cubic metres of dirigible fly by civil aviaton in fusion spatial domain
Office's management, remaining situation, including other flights including increasingly popular miniature aerial photography aircraft, managed by employer's organization,
Or be voluntarily responsible for by manipulator.
Existing unmanned plane landing platform is generally fixed platform, and the unmanned plane after landing stills need manually to be reclaimed, and is expended
Human cost, automaticity is low.
The content of the invention
The technical problems to be solved by the invention are existing unmanned plane landing platform mostly fixed platforms, nobody after landing
Machine stills need manually to be reclaimed, and labor intensive cost, automaticity is low, it is therefore intended that provides a kind of SUAV and reclaims
Understructure, it is generally fixed platform to solve existing unmanned plane landing platform, and the unmanned plane after landing stills need manually to be reclaimed,
Labor intensive cost, the low problem of automaticity.
The present invention is achieved through the following technical solutions：
A kind of SUAV reclaims understructure, including Landing stage and slide rail, and the Landing stage bottom is provided with fine setting
Device, Landing stage is connected by micromatic setting with slide assemblies, and slide assemblies are matched with slide rail.Unmanned plane is dropped on Landing stage
After, Landing stage is moved along slide rail, and unmanned plane directly is sent into hangar.
Position sensor and processor are additionally provided with the Landing stage, processor is filled with position sensor, fine setting respectively
Put and connected with slide assemblies；
Processor：The positional information that receiving position sensor sends, sends control signals to micromatic setting and cunning after treatment
Dynamic component；
Position sensor：The positional information of unmanned plane to be landed is gathered, positional information is sent to processor；
Micromatic setting：The control signal that receiving processor sends is acted；
Slide assemblies：The control signal that receiving processor sends is acted.Position sensor is detected treats landing unmanned plane
Relative to the position of position sensor, the position of unmanned plane is sent to processor, processor control micromatic setting and Slide Group
Part action makes Landing stage be located at the underface of unmanned plane, using said apparatus UAV Landing can be made in the center of Landing stage, protects
Stabilization of the card Landing stage during unmanned plane is sent into hangar.
The position sensor uses ultrasonic sensor.Detection is carried out in closer distance using ultrasonic sensor
Valency round-the-clock can be used, technology maturation than high.
The micromatic setting is that the gear that stepper motor drives is connected with slide assemblies.Using stepper motor and the group of gear
Close control accurate.
The present invention compared with prior art, has the following advantages and advantages：
1st, a kind of SUAV of the invention reclaims understructure, can be acted with the motion of unmanned plane, makes unmanned plane
The Landing stage center of landing；
2nd, a kind of SUAV of the invention reclaims understructure, and directly hangar can be sent into along slide rail after unmanned plane landing.
Brief description of the drawings
Accompanying drawing described herein is used for providing further understanding the embodiment of the present invention, constitutes of the application
Point, do not constitute the restriction to the embodiment of the present invention.In the accompanying drawings：
Fig. 1 is schematic structural view of the invention.
Mark and corresponding parts title in accompanying drawing：
1- unmanned planes, 2- undercarriages, 3- Landing stages, 4- position sensors, 5- processors, 6- micromatic settings, 7- Slide Groups
Part, 8- slide rails.
Specific embodiment
To make the object, technical solutions and advantages of the present invention become more apparent, with reference to embodiment and accompanying drawing, to this
Invention is described in further detail, and exemplary embodiment of the invention and its explanation are only used for explaining the present invention, do not make
It is limitation of the invention.
Embodiment
As shown in figure 1, a kind of SUAV of the invention reclaims understructure, including Landing stage 3 and slide rail 8, described
The bottom of table 3 is provided with micromatic setting 6, and Landing stage 3 is connected by micromatic setting 6 with slide assemblies 7, slide assemblies 7 and slide rail 8
Matching.After unmanned plane 1 is dropped to 3 on Landing stage, slide assemblies 7 drive Landing stage 3 to be moved along slide rail 8, directly by unmanned plane 1
Feeding hangar.3 are additionally provided with position sensor 4 and processor 5 on the Landing stage, and processor 5 uses AT89S52, processor 5
It is connected with position sensor 4, micromatic setting 6 and slide assemblies 7 respectively；The position sensor 4 uses ultrasonic sensor.
The micromatic setting 6 is that the gear that stepper motor drives is connected with slide assemblies.Position sensor 4 is detected treats landing unmanned plane 1
Relative to the position of position sensor 4, the position of unmanned plane 1 is sent to processor 5, processor 5 controls micromatic setting 6 and slides
Dynamic component 7 acts the underface for making Landing stage 3 be located at unmanned plane 1, and the drop 2 of unmanned plane 1 can be made using said apparatus
Land is in the center of Landing stage 3, it is ensured that stabilization of the Landing stage 3 during unmanned plane 1 is sent into hangar.Passed using ultrasonic wave simultaneously
Sensor is carried out detecting that cost performance is high in closer distance, round-the-clock can used, technology maturation.
Processor 5：The positional information that receiving position sensor 4 sends, sends control signals to the He of micromatic setting 6 after treatment
Slide assemblies 7；
Position sensor 4：The positional information of unmanned plane 1 to be landed is gathered, positional information is sent to processor 5；
Micromatic setting 6：The control signal that receiving processor 5 sends is acted；
Slide assemblies 7：The control signal that receiving processor 5 sends is acted.
Above-described specific embodiment, has been carried out further to the purpose of the present invention, technical scheme and beneficial effect
Describe in detail, should be understood that and the foregoing is only specific embodiment of the invention, be not intended to limit the present invention
Protection domain, all any modification, equivalent substitution and improvements within the spirit and principles in the present invention, done etc. all should include
Within protection scope of the present invention.
Claims (4)
1. a kind of SUAV reclaims understructure, including Landing stage (3) and slide rail (8), it is characterised in that the Landing stage
(3) bottom is provided with micromatic setting (6), and Landing stage (3) is connected by micromatic setting (6) with slide assemblies (7), slide assemblies
(7) matched with slide rail (8).
2. a kind of SUAV according to claim 1 reclaims understructure, it is characterised in that the Landing stage (3)
On be additionally provided with position sensor (4) and processor (5), processor (5) respectively with position sensor (4), micromatic setting (6) and
Slide assemblies (7) are connected；
Processor：The positional information that receiving position sensor sends, sends control signals to micromatic setting and Slide Group after treatment
Part；
Position sensor：The positional information of unmanned plane to be landed is gathered, positional information is sent to processor；
Micromatic setting：The control signal that receiving processor sends is acted；
Slide assemblies：The control signal that receiving processor sends is acted.
3. a kind of SUAV according to claim 1 reclaims understructure, it is characterised in that the position sensor
(4) ultrasonic sensor is used.
4. a kind of SUAV according to claim 1 reclaims understructure, it is characterised in that the micromatic setting
(6) for the gear that stepper motor drives is connected with slide assemblies.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710004602.8A CN106742016A (en) | 2017-01-04 | 2017-01-04 | A kind of SUAV reclaims understructure |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710004602.8A CN106742016A (en) | 2017-01-04 | 2017-01-04 | A kind of SUAV reclaims understructure |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106742016A true CN106742016A (en) | 2017-05-31 |
Family
ID=58950955
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710004602.8A Pending CN106742016A (en) | 2017-01-04 | 2017-01-04 | A kind of SUAV reclaims understructure |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106742016A (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109774961A (en) * | 2019-01-09 | 2019-05-21 | 徐工集团工程机械股份有限公司 | Unmanned plane draw off gear and its control method |
| CN111142554A (en) * | 2019-12-16 | 2020-05-12 | 南京业祥科技发展有限公司 | Automatic positioning landing control system and method for unmanned aerial vehicle |
| WO2024061095A1 (en) * | 2022-09-21 | 2024-03-28 | 亿航智能设备（广州）有限公司 | Adjustment device for aircraft entering hangar and hangar |
Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP2799336A1 (en) * | 2013-04-29 | 2014-11-05 | The Boeing Company | Device and method for use with unmanned aerial vehicles |
| CN204462852U (en) * | 2015-03-25 | 2015-07-08 | 成都好飞机器人科技有限公司 | For unmanned vehicle charging from motion tracking landing platform |
| WO2016059555A1 (en) * | 2014-10-13 | 2016-04-21 | Systems Engineering Associates Corporation | Systems and methods for deployment and operation of vertical take-off and landing (vtol) unmanned aerial vehicles |
| CN205440852U (en) * | 2016-03-16 | 2016-08-10 | 安徽钰龙信息科技有限公司 | A unmanned aerial vehicle descending base for command car |
| CN105863353A (en) * | 2016-06-09 | 2016-08-17 | 徐洪军 | Taking-off and landing supply robot of small unmanned aerial vehicle group |
| CN106005462A (en) * | 2016-06-29 | 2016-10-12 | 任雪峰 | Retraction system for mooring unmanned aerial vehicle and method for deploying and retracting mooring unmanned aerial vehicle with same |
| CN206502044U (en) * | 2017-01-04 | 2017-09-19 | 四川克瑞斯航空科技有限公司 | A kind of SUAV reclaims understructure |
-
2017
- 2017-01-04 CN CN201710004602.8A patent/CN106742016A/en active Pending
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP2799336A1 (en) * | 2013-04-29 | 2014-11-05 | The Boeing Company | Device and method for use with unmanned aerial vehicles |
| WO2016059555A1 (en) * | 2014-10-13 | 2016-04-21 | Systems Engineering Associates Corporation | Systems and methods for deployment and operation of vertical take-off and landing (vtol) unmanned aerial vehicles |
| CN204462852U (en) * | 2015-03-25 | 2015-07-08 | 成都好飞机器人科技有限公司 | For unmanned vehicle charging from motion tracking landing platform |
| CN205440852U (en) * | 2016-03-16 | 2016-08-10 | 安徽钰龙信息科技有限公司 | A unmanned aerial vehicle descending base for command car |
| CN105863353A (en) * | 2016-06-09 | 2016-08-17 | 徐洪军 | Taking-off and landing supply robot of small unmanned aerial vehicle group |
| CN106005462A (en) * | 2016-06-29 | 2016-10-12 | 任雪峰 | Retraction system for mooring unmanned aerial vehicle and method for deploying and retracting mooring unmanned aerial vehicle with same |
| CN206502044U (en) * | 2017-01-04 | 2017-09-19 | 四川克瑞斯航空科技有限公司 | A kind of SUAV reclaims understructure |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109774961A (en) * | 2019-01-09 | 2019-05-21 | 徐工集团工程机械股份有限公司 | Unmanned plane draw off gear and its control method |
| CN109774961B (en) * | 2019-01-09 | 2024-04-02 | 徐工集团工程机械股份有限公司 | Unmanned aerial vehicle retraction device and control method thereof |
| CN111142554A (en) * | 2019-12-16 | 2020-05-12 | 南京业祥科技发展有限公司 | Automatic positioning landing control system and method for unmanned aerial vehicle |
| WO2024061095A1 (en) * | 2022-09-21 | 2024-03-28 | 亿航智能设备（广州）有限公司 | Adjustment device for aircraft entering hangar and hangar |
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| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20170531 |
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| RJ01 | Rejection of invention patent application after publication |